Advanced search options

Advanced Search Options 🞨

Browse by author name (“Author name starts with…”).

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

You searched for subject:(Aircraft materials). Showing records 1 – 30 of 41 total matches.

[1] [2]

Search Limiters

Last 2 Years | English Only

▼ Search Limiters


Drexel University

1. Shields, David J. Determining the Dependence of Grain Boundary Mobility on Misorientation in High Purity Aluminum with Zirconium Additions.

Degree: 2013, Drexel University

 Aluminum alloys are used frequently for applications within the aerospace industry, creating a demand for finely tuned aluminum alloys that maximize a material property of… (more)

Subjects/Keywords: Materials science; Aluminum alloys; Aircraft industry

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Shields, D. J. (2013). Determining the Dependence of Grain Boundary Mobility on Misorientation in High Purity Aluminum with Zirconium Additions. (Thesis). Drexel University. Retrieved from http://hdl.handle.net/1860/4304

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Shields, David J. “Determining the Dependence of Grain Boundary Mobility on Misorientation in High Purity Aluminum with Zirconium Additions.” 2013. Thesis, Drexel University. Accessed May 20, 2019. http://hdl.handle.net/1860/4304.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Shields, David J. “Determining the Dependence of Grain Boundary Mobility on Misorientation in High Purity Aluminum with Zirconium Additions.” 2013. Web. 20 May 2019.

Vancouver:

Shields DJ. Determining the Dependence of Grain Boundary Mobility on Misorientation in High Purity Aluminum with Zirconium Additions. [Internet] [Thesis]. Drexel University; 2013. [cited 2019 May 20]. Available from: http://hdl.handle.net/1860/4304.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Shields DJ. Determining the Dependence of Grain Boundary Mobility on Misorientation in High Purity Aluminum with Zirconium Additions. [Thesis]. Drexel University; 2013. Available from: http://hdl.handle.net/1860/4304

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Australian National University

2. Bendemra, Hamza. Automation of Lay-Up in the Repair of Advanced Composite Aircraft Structures .

Degree: 2016, Australian National University

 The use of lightweight composite materials in aircraft structure has become increasingly widespread over the past thirty years as the need for reduced fuel consumption… (more)

Subjects/Keywords: composite materials; automated fibre placement; aircraft materials; scarf repair

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Bendemra, H. (2016). Automation of Lay-Up in the Repair of Advanced Composite Aircraft Structures . (Thesis). Australian National University. Retrieved from http://hdl.handle.net/1885/101713

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Bendemra, Hamza. “Automation of Lay-Up in the Repair of Advanced Composite Aircraft Structures .” 2016. Thesis, Australian National University. Accessed May 20, 2019. http://hdl.handle.net/1885/101713.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Bendemra, Hamza. “Automation of Lay-Up in the Repair of Advanced Composite Aircraft Structures .” 2016. Web. 20 May 2019.

Vancouver:

Bendemra H. Automation of Lay-Up in the Repair of Advanced Composite Aircraft Structures . [Internet] [Thesis]. Australian National University; 2016. [cited 2019 May 20]. Available from: http://hdl.handle.net/1885/101713.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Bendemra H. Automation of Lay-Up in the Repair of Advanced Composite Aircraft Structures . [Thesis]. Australian National University; 2016. Available from: http://hdl.handle.net/1885/101713

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Florida

3. Lacroix, Bradley W. On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles.

Degree: PhD, Mechanical Engineering - Mechanical and Aerospace Engineering, 2013, University of Florida

 This document details the research performed on applying piezoelectric macro fiber composite actuators on micro air vehicles. The research objective was to apply the minimum… (more)

Subjects/Keywords: Aircraft; Aircraft pitch; Aircraft roll; Aircraft wings; Carbon fibers; Design optimization; Geometry; Steels; Swept wings; Wind tunnels; composite  – fiber  – flying  – macro  – materials  – mav  – mfc  – morphing  – optimization  – piezoelectric  – smart  – uav  – wing

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Lacroix, B. W. (2013). On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0046212

Chicago Manual of Style (16th Edition):

Lacroix, Bradley W. “On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles.” 2013. Doctoral Dissertation, University of Florida. Accessed May 20, 2019. http://ufdc.ufl.edu/UFE0046212.

MLA Handbook (7th Edition):

Lacroix, Bradley W. “On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles.” 2013. Web. 20 May 2019.

Vancouver:

Lacroix BW. On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles. [Internet] [Doctoral dissertation]. University of Florida; 2013. [cited 2019 May 20]. Available from: http://ufdc.ufl.edu/UFE0046212.

Council of Science Editors:

Lacroix BW. On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles. [Doctoral Dissertation]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0046212


University of KwaZulu-Natal

4. Moore, Neall Neville. Lightweight structural design of UAV wing through the use of coreless composite materials employing novel construction techniques.

Degree: 2017, University of KwaZulu-Natal

 A new structural layout was designed for an existing UAV wing with the aims of lightening the wing by eliminating the use of cored composite… (more)

Subjects/Keywords: Theses - Mechanical Engineering.; Composite materials.; UAV.; FEA.; Lightweight.; Aircraft structural design.

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Moore, N. N. (2017). Lightweight structural design of UAV wing through the use of coreless composite materials employing novel construction techniques. (Thesis). University of KwaZulu-Natal. Retrieved from http://hdl.handle.net/10413/16174

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Moore, Neall Neville. “Lightweight structural design of UAV wing through the use of coreless composite materials employing novel construction techniques.” 2017. Thesis, University of KwaZulu-Natal. Accessed May 20, 2019. http://hdl.handle.net/10413/16174.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Moore, Neall Neville. “Lightweight structural design of UAV wing through the use of coreless composite materials employing novel construction techniques.” 2017. Web. 20 May 2019.

Vancouver:

Moore NN. Lightweight structural design of UAV wing through the use of coreless composite materials employing novel construction techniques. [Internet] [Thesis]. University of KwaZulu-Natal; 2017. [cited 2019 May 20]. Available from: http://hdl.handle.net/10413/16174.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Moore NN. Lightweight structural design of UAV wing through the use of coreless composite materials employing novel construction techniques. [Thesis]. University of KwaZulu-Natal; 2017. Available from: http://hdl.handle.net/10413/16174

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Florida

5. Bowland, Christopher C. Conformal Growth Method of Ferroelectric Materials for Multifunctional Composites.

Degree: PhD, Materials Science and Engineering, 2016, University of Florida

 Multifunctional composites are the next generation of composites and aim to simultaneously meet multiple performance objectives to create system-level performance enhancements. Current fiber-reinforced composites have… (more)

Subjects/Keywords: Acceleration; Aircraft; Aircraft wings; Carbon fibers; Composite materials; Electric potential; Nanowires; Polymers; Tensile strength; Titanium; carbon  – composite  – ferroelectric  – multifunctional  – nanowires

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Bowland, C. C. (2016). Conformal Growth Method of Ferroelectric Materials for Multifunctional Composites. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0049854

Chicago Manual of Style (16th Edition):

Bowland, Christopher C. “Conformal Growth Method of Ferroelectric Materials for Multifunctional Composites.” 2016. Doctoral Dissertation, University of Florida. Accessed May 20, 2019. http://ufdc.ufl.edu/UFE0049854.

MLA Handbook (7th Edition):

Bowland, Christopher C. “Conformal Growth Method of Ferroelectric Materials for Multifunctional Composites.” 2016. Web. 20 May 2019.

Vancouver:

Bowland CC. Conformal Growth Method of Ferroelectric Materials for Multifunctional Composites. [Internet] [Doctoral dissertation]. University of Florida; 2016. [cited 2019 May 20]. Available from: http://ufdc.ufl.edu/UFE0049854.

Council of Science Editors:

Bowland CC. Conformal Growth Method of Ferroelectric Materials for Multifunctional Composites. [Doctoral Dissertation]. University of Florida; 2016. Available from: http://ufdc.ufl.edu/UFE0049854

6. Jiby, K. Gopinath. Theoretical Design and Synthesis of Donor-Acceptor Conjugated Polymers for Photovoltaic and NLO Applications.

Degree: 2015, Cochin University of Science and Technology

Polymers with conjugated π-electron backbone display unusual electronic properties such as low energy optical transition, low ionization potentials, and high electron affinities. The properties that… (more)

Subjects/Keywords: Polymers; Electronic Transmission; electromagnetic interference (EMI),; conjugated polymer materials; diodes; aircraft structures

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Jiby, K. G. (2015). Theoretical Design and Synthesis of Donor-Acceptor Conjugated Polymers for Photovoltaic and NLO Applications. (Thesis). Cochin University of Science and Technology. Retrieved from http://dyuthi.cusat.ac.in/purl/5055

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Jiby, K Gopinath. “Theoretical Design and Synthesis of Donor-Acceptor Conjugated Polymers for Photovoltaic and NLO Applications.” 2015. Thesis, Cochin University of Science and Technology. Accessed May 20, 2019. http://dyuthi.cusat.ac.in/purl/5055.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Jiby, K Gopinath. “Theoretical Design and Synthesis of Donor-Acceptor Conjugated Polymers for Photovoltaic and NLO Applications.” 2015. Web. 20 May 2019.

Vancouver:

Jiby KG. Theoretical Design and Synthesis of Donor-Acceptor Conjugated Polymers for Photovoltaic and NLO Applications. [Internet] [Thesis]. Cochin University of Science and Technology; 2015. [cited 2019 May 20]. Available from: http://dyuthi.cusat.ac.in/purl/5055.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Jiby KG. Theoretical Design and Synthesis of Donor-Acceptor Conjugated Polymers for Photovoltaic and NLO Applications. [Thesis]. Cochin University of Science and Technology; 2015. Available from: http://dyuthi.cusat.ac.in/purl/5055

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Dayton

7. O'Grady, Brendan. Multi-Objective Optimization of a Three Cell Morphing Wing Substructure.

Degree: MS(M.S.), Mechanical Engineering, 2010, University of Dayton

 This thesis investigates the application of distributed actuation within a flexible morphing wingstructure through experimentation and optimization techniques. The goal is to understand the effectthat… (more)

Subjects/Keywords: Aerospace Materials; Engineering; Aircraft design; mechanisms; wing morphing; optimization; matlab; dynamic simulation; adams; nastran

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

O'Grady, B. (2010). Multi-Objective Optimization of a Three Cell Morphing Wing Substructure. (Masters Thesis). University of Dayton. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=dayton1272483780

Chicago Manual of Style (16th Edition):

O'Grady, Brendan. “Multi-Objective Optimization of a Three Cell Morphing Wing Substructure.” 2010. Masters Thesis, University of Dayton. Accessed May 20, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1272483780.

MLA Handbook (7th Edition):

O'Grady, Brendan. “Multi-Objective Optimization of a Three Cell Morphing Wing Substructure.” 2010. Web. 20 May 2019.

Vancouver:

O'Grady B. Multi-Objective Optimization of a Three Cell Morphing Wing Substructure. [Internet] [Masters thesis]. University of Dayton; 2010. [cited 2019 May 20]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1272483780.

Council of Science Editors:

O'Grady B. Multi-Objective Optimization of a Three Cell Morphing Wing Substructure. [Masters Thesis]. University of Dayton; 2010. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1272483780

8. Κοτζακόλιος, Αθανάσιος. Blast response of aircraft structures.

Degree: 2011, University of Patras

The scope of this project is the realization of composite and hybrid sub-aerostructures which exhibit superior blast performance compared to reference composite and hybrid substructures.… (more)

Subjects/Keywords: Blast; Composite materials; Aircraft; Finite element analysis; 629.134 5; Έκρηξη; Σύνθετα υλικά

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Κοτζακόλιος, . (2011). Blast response of aircraft structures. (Doctoral Dissertation). University of Patras. Retrieved from http://hdl.handle.net/10889/5068

Chicago Manual of Style (16th Edition):

Κοτζακόλιος, Αθανάσιος. “Blast response of aircraft structures.” 2011. Doctoral Dissertation, University of Patras. Accessed May 20, 2019. http://hdl.handle.net/10889/5068.

MLA Handbook (7th Edition):

Κοτζακόλιος, Αθανάσιος. “Blast response of aircraft structures.” 2011. Web. 20 May 2019.

Vancouver:

Κοτζακόλιος . Blast response of aircraft structures. [Internet] [Doctoral dissertation]. University of Patras; 2011. [cited 2019 May 20]. Available from: http://hdl.handle.net/10889/5068.

Council of Science Editors:

Κοτζακόλιος . Blast response of aircraft structures. [Doctoral Dissertation]. University of Patras; 2011. Available from: http://hdl.handle.net/10889/5068


University of Cincinnati

9. Shekhar, Anjali. Study and Numerical Simulation of Unconventional Engine Technology.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2018, University of Cincinnati

 The aim of this thesis is to understand the working of two unconventional aircraft propulsionsystems and to setup a two-dimensional transient simulation to analyze its… (more)

Subjects/Keywords: Aerospace Materials; Aircraft Propulsion; Computational Fluid Dynamics; Pressure Gain Combustion; Pulsejets; Transient Simulation

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Shekhar, A. (2018). Study and Numerical Simulation of Unconventional Engine Technology. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1544098607675961

Chicago Manual of Style (16th Edition):

Shekhar, Anjali. “Study and Numerical Simulation of Unconventional Engine Technology.” 2018. Masters Thesis, University of Cincinnati. Accessed May 20, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1544098607675961.

MLA Handbook (7th Edition):

Shekhar, Anjali. “Study and Numerical Simulation of Unconventional Engine Technology.” 2018. Web. 20 May 2019.

Vancouver:

Shekhar A. Study and Numerical Simulation of Unconventional Engine Technology. [Internet] [Masters thesis]. University of Cincinnati; 2018. [cited 2019 May 20]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1544098607675961.

Council of Science Editors:

Shekhar A. Study and Numerical Simulation of Unconventional Engine Technology. [Masters Thesis]. University of Cincinnati; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1544098607675961


Cal Poly

10. Lazarin, Juan Reuben. OPTIMUM DESIGN OF COMPOSITE WING SPAR SUBJECTED TO FATIGUE LOADINGS.

Degree: MS, Aerospace Engineering, 2017, Cal Poly

  Composites are now being incorporated into aircraft designs because of their high strength to weight ratio compared to traditional metal materials. Due to the… (more)

Subjects/Keywords: Composite; Fatigue; Strain Gages; Wing; Aircraft; Finite Element Analysis; Structures and Materials

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Lazarin, J. R. (2017). OPTIMUM DESIGN OF COMPOSITE WING SPAR SUBJECTED TO FATIGUE LOADINGS. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1816

Chicago Manual of Style (16th Edition):

Lazarin, Juan Reuben. “OPTIMUM DESIGN OF COMPOSITE WING SPAR SUBJECTED TO FATIGUE LOADINGS.” 2017. Masters Thesis, Cal Poly. Accessed May 20, 2019. https://digitalcommons.calpoly.edu/theses/1816.

MLA Handbook (7th Edition):

Lazarin, Juan Reuben. “OPTIMUM DESIGN OF COMPOSITE WING SPAR SUBJECTED TO FATIGUE LOADINGS.” 2017. Web. 20 May 2019.

Vancouver:

Lazarin JR. OPTIMUM DESIGN OF COMPOSITE WING SPAR SUBJECTED TO FATIGUE LOADINGS. [Internet] [Masters thesis]. Cal Poly; 2017. [cited 2019 May 20]. Available from: https://digitalcommons.calpoly.edu/theses/1816.

Council of Science Editors:

Lazarin JR. OPTIMUM DESIGN OF COMPOSITE WING SPAR SUBJECTED TO FATIGUE LOADINGS. [Masters Thesis]. Cal Poly; 2017. Available from: https://digitalcommons.calpoly.edu/theses/1816


University of KwaZulu-Natal

11. Vugampore, Jean-Marie Vianney. Development of high strength material for smart aircraft bolt.

Degree: PhD, Mechanical engineering, 2005, University of KwaZulu-Natal

 Scientists are constantly seeking new and convenient non-destructive damage assessment techniques. In fact, a global market has developed for structural health monitoring products. Many of… (more)

Subjects/Keywords: Mechanical engineering.; Strength of materials.; Smart materials.; Aircraft steel.

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Vugampore, J. V. (2005). Development of high strength material for smart aircraft bolt. (Doctoral Dissertation). University of KwaZulu-Natal. Retrieved from http://hdl.handle.net/10413/2835

Chicago Manual of Style (16th Edition):

Vugampore, Jean-Marie Vianney. “Development of high strength material for smart aircraft bolt.” 2005. Doctoral Dissertation, University of KwaZulu-Natal. Accessed May 20, 2019. http://hdl.handle.net/10413/2835.

MLA Handbook (7th Edition):

Vugampore, Jean-Marie Vianney. “Development of high strength material for smart aircraft bolt.” 2005. Web. 20 May 2019.

Vancouver:

Vugampore JV. Development of high strength material for smart aircraft bolt. [Internet] [Doctoral dissertation]. University of KwaZulu-Natal; 2005. [cited 2019 May 20]. Available from: http://hdl.handle.net/10413/2835.

Council of Science Editors:

Vugampore JV. Development of high strength material for smart aircraft bolt. [Doctoral Dissertation]. University of KwaZulu-Natal; 2005. Available from: http://hdl.handle.net/10413/2835


Indian Institute of Science

12. Shetty, Kishora. Ion-Nitriding Of Maraging Steel (MDN 250A Grade) For Light Combat Aircraft Applications.

Degree: 2007, Indian Institute of Science

 Maraging steels have got high strength and good toughness. Maraging steel MDN 250A grade is used for slat tracks on the leading edge of the… (more)

Subjects/Keywords: Steel; Light Combat Aircraft; Ion Nitriding; Maraging Steels - Physical Metallurgy; Ion-Nitrided Steels; Maraging Steels - Properties; Nitrided Samples; Materials Science

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Shetty, K. (2007). Ion-Nitriding Of Maraging Steel (MDN 250A Grade) For Light Combat Aircraft Applications. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/494

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Shetty, Kishora. “Ion-Nitriding Of Maraging Steel (MDN 250A Grade) For Light Combat Aircraft Applications.” 2007. Thesis, Indian Institute of Science. Accessed May 20, 2019. http://hdl.handle.net/2005/494.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Shetty, Kishora. “Ion-Nitriding Of Maraging Steel (MDN 250A Grade) For Light Combat Aircraft Applications.” 2007. Web. 20 May 2019.

Vancouver:

Shetty K. Ion-Nitriding Of Maraging Steel (MDN 250A Grade) For Light Combat Aircraft Applications. [Internet] [Thesis]. Indian Institute of Science; 2007. [cited 2019 May 20]. Available from: http://hdl.handle.net/2005/494.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Shetty K. Ion-Nitriding Of Maraging Steel (MDN 250A Grade) For Light Combat Aircraft Applications. [Thesis]. Indian Institute of Science; 2007. Available from: http://hdl.handle.net/2005/494

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

13. Kaloyanova, Valentina B. Structural Modeling and Optimization of a Joined-Wing Configuration of a High-Altitude Long-Endurance (HALE) Aircraft.

Degree: PhD, Engineering : Aerospace Engineering, 2009, University of Cincinnati

  Recent research trends have indicated an interest in High-Altitude, Long-Endurance (HALE) aircraft as a low-cost alternative to certain space missions, such as telecommunication relay,… (more)

Subjects/Keywords: Aerospace Materials; HALE Aircraft; joined-wing

…97 6.2.1. Overview of Aircraft Wing Design …...97 6.2.2. Description of the… …configuration with joined wings . 25 Fig. 1c. Example of an advanced UAV HALE Aircraft… …27 Fig. 1e. Results of group dominance in aircraft design . 29 Fig. 2… …operating costs. For these applications, the aircraft must fly at low speed in the stratosphere at… …the added fuel and equipment stored in the wings, the total aircraft weight is increased… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Kaloyanova, V. B. (2009). Structural Modeling and Optimization of a Joined-Wing Configuration of a High-Altitude Long-Endurance (HALE) Aircraft. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1259075776

Chicago Manual of Style (16th Edition):

Kaloyanova, Valentina B. “Structural Modeling and Optimization of a Joined-Wing Configuration of a High-Altitude Long-Endurance (HALE) Aircraft.” 2009. Doctoral Dissertation, University of Cincinnati. Accessed May 20, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1259075776.

MLA Handbook (7th Edition):

Kaloyanova, Valentina B. “Structural Modeling and Optimization of a Joined-Wing Configuration of a High-Altitude Long-Endurance (HALE) Aircraft.” 2009. Web. 20 May 2019.

Vancouver:

Kaloyanova VB. Structural Modeling and Optimization of a Joined-Wing Configuration of a High-Altitude Long-Endurance (HALE) Aircraft. [Internet] [Doctoral dissertation]. University of Cincinnati; 2009. [cited 2019 May 20]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1259075776.

Council of Science Editors:

Kaloyanova VB. Structural Modeling and Optimization of a Joined-Wing Configuration of a High-Altitude Long-Endurance (HALE) Aircraft. [Doctoral Dissertation]. University of Cincinnati; 2009. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1259075776


Wright State University

14. Dwire, Heather B. RISK BASED ANALYSIS AND DESIGN OF STIFFENED PLATES.

Degree: MSEgr, Mechanical Engineering, 2008, Wright State University

  The traditional Risk Based Design (RBD) process involves designing a structure based on risk estimates obtained during several iterations of an optimization routine. This… (more)

Subjects/Keywords: Aerospace Materials; Engineering; Mechanical Engineering; Aircraft Design; Risk Based Design; reliability-based optimization; Probability Distribution Function (PDF)

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Dwire, H. B. (2008). RISK BASED ANALYSIS AND DESIGN OF STIFFENED PLATES. (Masters Thesis). Wright State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=wright1208453129

Chicago Manual of Style (16th Edition):

Dwire, Heather B. “RISK BASED ANALYSIS AND DESIGN OF STIFFENED PLATES.” 2008. Masters Thesis, Wright State University. Accessed May 20, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=wright1208453129.

MLA Handbook (7th Edition):

Dwire, Heather B. “RISK BASED ANALYSIS AND DESIGN OF STIFFENED PLATES.” 2008. Web. 20 May 2019.

Vancouver:

Dwire HB. RISK BASED ANALYSIS AND DESIGN OF STIFFENED PLATES. [Internet] [Masters thesis]. Wright State University; 2008. [cited 2019 May 20]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1208453129.

Council of Science Editors:

Dwire HB. RISK BASED ANALYSIS AND DESIGN OF STIFFENED PLATES. [Masters Thesis]. Wright State University; 2008. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1208453129


Ohio University

15. Rose, Isaac D. Aerodynamic Modeling of an Unmanned Aerial Vehicle Using a Computational Fluid Dynamics Prediction Code.

Degree: MS, Electrical Engineering (Engineering and Technology), 2009, Ohio University

 The process of creating a six degree-of-freedom model for an aerospace vehicle requires detailed knowledge of the aerodynamic characteristics. This thesis presents an implementation of… (more)

Subjects/Keywords: Aerospace Materials; Electrical Engineering; Engineering; Brumby; Computational Fluid Dynamics; DATCOM; Missile DATCOM; Aerodynamic Coefficients; Aircraft Model; six degree-of-freedom model

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Rose, I. D. (2009). Aerodynamic Modeling of an Unmanned Aerial Vehicle Using a Computational Fluid Dynamics Prediction Code. (Masters Thesis). Ohio University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1237481460

Chicago Manual of Style (16th Edition):

Rose, Isaac D. “Aerodynamic Modeling of an Unmanned Aerial Vehicle Using a Computational Fluid Dynamics Prediction Code.” 2009. Masters Thesis, Ohio University. Accessed May 20, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1237481460.

MLA Handbook (7th Edition):

Rose, Isaac D. “Aerodynamic Modeling of an Unmanned Aerial Vehicle Using a Computational Fluid Dynamics Prediction Code.” 2009. Web. 20 May 2019.

Vancouver:

Rose ID. Aerodynamic Modeling of an Unmanned Aerial Vehicle Using a Computational Fluid Dynamics Prediction Code. [Internet] [Masters thesis]. Ohio University; 2009. [cited 2019 May 20]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1237481460.

Council of Science Editors:

Rose ID. Aerodynamic Modeling of an Unmanned Aerial Vehicle Using a Computational Fluid Dynamics Prediction Code. [Masters Thesis]. Ohio University; 2009. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1237481460


Universitat de Girona

16. Renart Canalias, Jordi. Desarrollo de un nuevo ensayo experimental para la evaluación de la calidad de uniones adhesivas entre componentes estructurales de composite para la indústria aeronáutica.

Degree: Departament d'Enginyeria Mecànica i de la Construcció Industrial, 2010, Universitat de Girona

 The use of composite materials in the aircraft industry has been increasing in recent years due to their application in structural parts. To reduce the… (more)

Subjects/Keywords: Composite materials; Composites; Compòsits; Aircraft industry; Industria aeronautica; Adhesive joints; Uniones adhesivas; Unions adhesives; Wedge; Cuña; Cunya; Delamination; Delaminación; Delaminació; 629

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Renart Canalias, J. (2010). Desarrollo de un nuevo ensayo experimental para la evaluación de la calidad de uniones adhesivas entre componentes estructurales de composite para la indústria aeronáutica. (Thesis). Universitat de Girona. Retrieved from http://hdl.handle.net/10803/296679

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Renart Canalias, Jordi. “Desarrollo de un nuevo ensayo experimental para la evaluación de la calidad de uniones adhesivas entre componentes estructurales de composite para la indústria aeronáutica.” 2010. Thesis, Universitat de Girona. Accessed May 20, 2019. http://hdl.handle.net/10803/296679.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Renart Canalias, Jordi. “Desarrollo de un nuevo ensayo experimental para la evaluación de la calidad de uniones adhesivas entre componentes estructurales de composite para la indústria aeronáutica.” 2010. Web. 20 May 2019.

Vancouver:

Renart Canalias J. Desarrollo de un nuevo ensayo experimental para la evaluación de la calidad de uniones adhesivas entre componentes estructurales de composite para la indústria aeronáutica. [Internet] [Thesis]. Universitat de Girona; 2010. [cited 2019 May 20]. Available from: http://hdl.handle.net/10803/296679.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Renart Canalias J. Desarrollo de un nuevo ensayo experimental para la evaluación de la calidad de uniones adhesivas entre componentes estructurales de composite para la indústria aeronáutica. [Thesis]. Universitat de Girona; 2010. Available from: http://hdl.handle.net/10803/296679

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Cornell University

17. Manzo, Justin. Analysis and Design of a Hyper-Elliptical Cambered Span Morphing Aircraft Wing .

Degree: 2006, Cornell University

 Morphing aircraft are a focus today due to their ability to combine multiple mission flexibility with a single vehicle. The Hyper-Elliptical Cambered Span (HECS) wing… (more)

Subjects/Keywords: morphing aircraft; HECS; smart materials; wing morphology; SMA

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Manzo, J. (2006). Analysis and Design of a Hyper-Elliptical Cambered Span Morphing Aircraft Wing . (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/3210

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Manzo, Justin. “Analysis and Design of a Hyper-Elliptical Cambered Span Morphing Aircraft Wing .” 2006. Thesis, Cornell University. Accessed May 20, 2019. http://hdl.handle.net/1813/3210.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Manzo, Justin. “Analysis and Design of a Hyper-Elliptical Cambered Span Morphing Aircraft Wing .” 2006. Web. 20 May 2019.

Vancouver:

Manzo J. Analysis and Design of a Hyper-Elliptical Cambered Span Morphing Aircraft Wing . [Internet] [Thesis]. Cornell University; 2006. [cited 2019 May 20]. Available from: http://hdl.handle.net/1813/3210.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Manzo J. Analysis and Design of a Hyper-Elliptical Cambered Span Morphing Aircraft Wing . [Thesis]. Cornell University; 2006. Available from: http://hdl.handle.net/1813/3210

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Indian Institute of Science

18. Sudha, J. Fatigue Damage Characterization Of Carbon/Epoxy Laminates Under Spectrum Loading.

Degree: 2007, Indian Institute of Science

 Fibre Reinforced Polymer Composites are extensively used in aircraft structures because of its high specific stiffness, high specific strength and tailorability. Though Fibre Reinforced Polymers… (more)

Subjects/Keywords: Carbon/Epoxy Laminates - Fatigue; Carbon Fiber Reinforced Polymer Laminates; Carbon Fibre Reinforced Epoxy Composites; Aircraft-Composite Structures - Fatigue; Aerospace Materials - Fatigue; Dynamic Mechanical Analysis; Materials Science

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Sudha, J. (2007). Fatigue Damage Characterization Of Carbon/Epoxy Laminates Under Spectrum Loading. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2257

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Sudha, J. “Fatigue Damage Characterization Of Carbon/Epoxy Laminates Under Spectrum Loading.” 2007. Thesis, Indian Institute of Science. Accessed May 20, 2019. http://hdl.handle.net/2005/2257.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Sudha, J. “Fatigue Damage Characterization Of Carbon/Epoxy Laminates Under Spectrum Loading.” 2007. Web. 20 May 2019.

Vancouver:

Sudha J. Fatigue Damage Characterization Of Carbon/Epoxy Laminates Under Spectrum Loading. [Internet] [Thesis]. Indian Institute of Science; 2007. [cited 2019 May 20]. Available from: http://hdl.handle.net/2005/2257.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Sudha J. Fatigue Damage Characterization Of Carbon/Epoxy Laminates Under Spectrum Loading. [Thesis]. Indian Institute of Science; 2007. Available from: http://hdl.handle.net/2005/2257

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

19. Clermont, Paul Daniel Stanley. Characterization and prediction of flow electrification phenomena in fuel tanks of aeronautical structures : Caractérisation et prédiction des phénomènes d'électrisation par écoulement dans lesréservoirs de carburant de structures aéronautiques.

Degree: Docteur es, Génie électrique et mécanique des milieux fluides, 2016, Poitiers

Avec la nouvelle génération d'avions composites, une attention est portée sur les systèmes de carburant vis-à-vis de la prévention des décharges électrostatiques (ESD) durant les… (more)

Subjects/Keywords: Électrisation par écoulement; Décharge électrostatique; Matériaux composites; Réservoir de carburant aéronautique; Carburant avionique; Flow electrification; Electrostatic discharge; Composite materials; Aircraft fuel tank; Aviation fuel; 621.3

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Clermont, P. D. S. (2016). Characterization and prediction of flow electrification phenomena in fuel tanks of aeronautical structures : Caractérisation et prédiction des phénomènes d'électrisation par écoulement dans lesréservoirs de carburant de structures aéronautiques. (Doctoral Dissertation). Poitiers. Retrieved from http://www.theses.fr/2016POIT2258

Chicago Manual of Style (16th Edition):

Clermont, Paul Daniel Stanley. “Characterization and prediction of flow electrification phenomena in fuel tanks of aeronautical structures : Caractérisation et prédiction des phénomènes d'électrisation par écoulement dans lesréservoirs de carburant de structures aéronautiques.” 2016. Doctoral Dissertation, Poitiers. Accessed May 20, 2019. http://www.theses.fr/2016POIT2258.

MLA Handbook (7th Edition):

Clermont, Paul Daniel Stanley. “Characterization and prediction of flow electrification phenomena in fuel tanks of aeronautical structures : Caractérisation et prédiction des phénomènes d'électrisation par écoulement dans lesréservoirs de carburant de structures aéronautiques.” 2016. Web. 20 May 2019.

Vancouver:

Clermont PDS. Characterization and prediction of flow electrification phenomena in fuel tanks of aeronautical structures : Caractérisation et prédiction des phénomènes d'électrisation par écoulement dans lesréservoirs de carburant de structures aéronautiques. [Internet] [Doctoral dissertation]. Poitiers; 2016. [cited 2019 May 20]. Available from: http://www.theses.fr/2016POIT2258.

Council of Science Editors:

Clermont PDS. Characterization and prediction of flow electrification phenomena in fuel tanks of aeronautical structures : Caractérisation et prédiction des phénomènes d'électrisation par écoulement dans lesréservoirs de carburant de structures aéronautiques. [Doctoral Dissertation]. Poitiers; 2016. Available from: http://www.theses.fr/2016POIT2258


Université de Bordeaux I

20. Griesser, Aurélia. Réalisation de matériaux composites à conductivité thermique accrue pour l’aéronautique : Enhanced SiC/SiC composites for high temperature applications.

Degree: Docteur es, Physico-Chimie de la Matière Condensée, 2012, Université de Bordeaux I

Pour réduire les nuisances et pollutions émises par le transport aérien, une solution consisterait à remplacer les matériaux des pièces chaudes des moteurs d'avions par… (more)

Subjects/Keywords: Composite; Slurry cast MI; Aéronautique; Moteur d'avion; Haute température; Matériaux; Cmc; Composite; Slurry cast MI; Aeronautic; Aircraft engine; High temperature; Materials; Cmc

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Griesser, A. (2012). Réalisation de matériaux composites à conductivité thermique accrue pour l’aéronautique : Enhanced SiC/SiC composites for high temperature applications. (Doctoral Dissertation). Université de Bordeaux I. Retrieved from http://www.theses.fr/2012BOR14699

Chicago Manual of Style (16th Edition):

Griesser, Aurélia. “Réalisation de matériaux composites à conductivité thermique accrue pour l’aéronautique : Enhanced SiC/SiC composites for high temperature applications.” 2012. Doctoral Dissertation, Université de Bordeaux I. Accessed May 20, 2019. http://www.theses.fr/2012BOR14699.

MLA Handbook (7th Edition):

Griesser, Aurélia. “Réalisation de matériaux composites à conductivité thermique accrue pour l’aéronautique : Enhanced SiC/SiC composites for high temperature applications.” 2012. Web. 20 May 2019.

Vancouver:

Griesser A. Réalisation de matériaux composites à conductivité thermique accrue pour l’aéronautique : Enhanced SiC/SiC composites for high temperature applications. [Internet] [Doctoral dissertation]. Université de Bordeaux I; 2012. [cited 2019 May 20]. Available from: http://www.theses.fr/2012BOR14699.

Council of Science Editors:

Griesser A. Réalisation de matériaux composites à conductivité thermique accrue pour l’aéronautique : Enhanced SiC/SiC composites for high temperature applications. [Doctoral Dissertation]. Université de Bordeaux I; 2012. Available from: http://www.theses.fr/2012BOR14699

21. Perrino, Michael. An Experimental Study into Pylon, Wing, and Flap Installation Effects on Jet Noise Generated by Commercial Aircraft.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2014, University of Cincinnati

 A pylon bottom bifurcation and a wing with variable flaps were designed and builtto attach to a scaled model of a coaxial exhaust nozzle system.… (more)

Subjects/Keywords: Aerospace Materials; Aeroacoustics; Aircraft Engine; Pylon; Noise; Nozzle

aircraft tend to be situated in the vicinity of dense populations and the increase in noise has… …aircraft currently have to meet the Stage-3 requirements of the Federal Aviation Regulations… …that aircraft must achieve in order to be used. It is important that airframe and aircraft… …1.1 Aircraft Noise There are several sources of aircraft noise that must be considered… …individually in order to reduce the total noise of an aircraft. The main sources of noise generated… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Perrino, M. (2014). An Experimental Study into Pylon, Wing, and Flap Installation Effects on Jet Noise Generated by Commercial Aircraft. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1406819764

Chicago Manual of Style (16th Edition):

Perrino, Michael. “An Experimental Study into Pylon, Wing, and Flap Installation Effects on Jet Noise Generated by Commercial Aircraft.” 2014. Doctoral Dissertation, University of Cincinnati. Accessed May 20, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1406819764.

MLA Handbook (7th Edition):

Perrino, Michael. “An Experimental Study into Pylon, Wing, and Flap Installation Effects on Jet Noise Generated by Commercial Aircraft.” 2014. Web. 20 May 2019.

Vancouver:

Perrino M. An Experimental Study into Pylon, Wing, and Flap Installation Effects on Jet Noise Generated by Commercial Aircraft. [Internet] [Doctoral dissertation]. University of Cincinnati; 2014. [cited 2019 May 20]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1406819764.

Council of Science Editors:

Perrino M. An Experimental Study into Pylon, Wing, and Flap Installation Effects on Jet Noise Generated by Commercial Aircraft. [Doctoral Dissertation]. University of Cincinnati; 2014. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1406819764

22. Mohin, Ma. Fatigue crack growth assessment and fatigue resistance enhancement of aluminium alloys.

Degree: PhD, 2018, University of Hertfordshire

 Fatigue damage of aluminium alloys is one of the key concerns in transport industries, particularly in the aerospace industry. The purpose of the project is… (more)

Subjects/Keywords: Fatigue; Fracture mechanics; Fatigue crack growth; Crack closure; Overload; Strip yield model; Fatigue crack growth threshold; Electromagnetic treatment; Electropulsing; Aluminium alloy; Aerostructure; Aircraft materials

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Mohin, M. (2018). Fatigue crack growth assessment and fatigue resistance enhancement of aluminium alloys. (Doctoral Dissertation). University of Hertfordshire. Retrieved from http://hdl.handle.net/2299/20824

Chicago Manual of Style (16th Edition):

Mohin, Ma. “Fatigue crack growth assessment and fatigue resistance enhancement of aluminium alloys.” 2018. Doctoral Dissertation, University of Hertfordshire. Accessed May 20, 2019. http://hdl.handle.net/2299/20824.

MLA Handbook (7th Edition):

Mohin, Ma. “Fatigue crack growth assessment and fatigue resistance enhancement of aluminium alloys.” 2018. Web. 20 May 2019.

Vancouver:

Mohin M. Fatigue crack growth assessment and fatigue resistance enhancement of aluminium alloys. [Internet] [Doctoral dissertation]. University of Hertfordshire; 2018. [cited 2019 May 20]. Available from: http://hdl.handle.net/2299/20824.

Council of Science Editors:

Mohin M. Fatigue crack growth assessment and fatigue resistance enhancement of aluminium alloys. [Doctoral Dissertation]. University of Hertfordshire; 2018. Available from: http://hdl.handle.net/2299/20824


Universitat de Girona

23. Badalló i Cañellas, Pere. Analysis and optimization of composite stringers.

Degree: Departament d'Enginyeria Mecànica i de la Construcció Industrial, 2015, Universitat de Girona

 L'ús de panells rigiditzats a la indústria aeronàutica i aeroespacial ha anat creixent les darreres dècades. Per altra banda, el creixement exponencial de l'ús dels… (more)

Subjects/Keywords: Panells rigiditzats; Stiffened panels; Paneles rigidizados; Materials compòsits; Composite materials; Materiales compuestos; Metamodelatge; Metamodeling; Metamodelado; Mètode dels elements finits; Finite element method; Método de los elementos finitos; Assaig virtual; Virtual test; Ensayo virtual; Aircraft industry; Industria aeronautica; Indústries aeroespacials; Aerospace industries; Indústrias aeroespaciales; 620; 629

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Badalló i Cañellas, P. (2015). Analysis and optimization of composite stringers. (Thesis). Universitat de Girona. Retrieved from http://hdl.handle.net/10803/323087

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Badalló i Cañellas, Pere. “Analysis and optimization of composite stringers.” 2015. Thesis, Universitat de Girona. Accessed May 20, 2019. http://hdl.handle.net/10803/323087.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Badalló i Cañellas, Pere. “Analysis and optimization of composite stringers.” 2015. Web. 20 May 2019.

Vancouver:

Badalló i Cañellas P. Analysis and optimization of composite stringers. [Internet] [Thesis]. Universitat de Girona; 2015. [cited 2019 May 20]. Available from: http://hdl.handle.net/10803/323087.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Badalló i Cañellas P. Analysis and optimization of composite stringers. [Thesis]. Universitat de Girona; 2015. Available from: http://hdl.handle.net/10803/323087

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Canterbury

24. McSwain, RH. Failure analysis of a brazed, stainless steel fuel injection line.

Degree: 2018, University of Canterbury

 An aircraft fuel line was found to have fractured and caused an in-flight fire. A brief history of the general problem of cracking in brazed… (more)

Subjects/Keywords: Field of Research::09 - Engineering::0912 - Materials Engineering::091207 - Metals and Alloy Materials; Field of Research::09 - Engineering::0913 - Mechanical Engineering; Field of Research::09 - Engineering::0901 - Aerospace Engineering::090104 - Aircraft Performance and Flight Control Systems

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

McSwain, R. (2018). Failure analysis of a brazed, stainless steel fuel injection line. (Thesis). University of Canterbury. Retrieved from http://hdl.handle.net/10092/15660

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

McSwain, RH. “Failure analysis of a brazed, stainless steel fuel injection line.” 2018. Thesis, University of Canterbury. Accessed May 20, 2019. http://hdl.handle.net/10092/15660.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

McSwain, RH. “Failure analysis of a brazed, stainless steel fuel injection line.” 2018. Web. 20 May 2019.

Vancouver:

McSwain R. Failure analysis of a brazed, stainless steel fuel injection line. [Internet] [Thesis]. University of Canterbury; 2018. [cited 2019 May 20]. Available from: http://hdl.handle.net/10092/15660.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

McSwain R. Failure analysis of a brazed, stainless steel fuel injection line. [Thesis]. University of Canterbury; 2018. Available from: http://hdl.handle.net/10092/15660

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

25. Van der Westhuizen, Artho Otto. Impact response of a continuous fibre reinforced thermoplastic from a soft bodied projectile.

Degree: MScEng, Mechanical and Mechatronic Engineering, 2013, Stellenbosch University

AFRIKAANSE OPSOMMING: Saamgestelde materiale het baie gewilde materiale in die lugvaart- en motor industrië geword as gevolg van die gewigsbesparende voordele wat dit inhou. Kostes… (more)

Subjects/Keywords: Mechanical engineering; Thermoplastic composites; Aircraft components  – Plastics; Composite materials; Thermoplastics  – Strength of materials; Thermoplastics  – Impact testing

…Chapter 1 Introduction Composite materials have become more popular over the years. Composites… …offer many advantages over traditional metallic materials due to their attractive stiffness to… …materials where fuel savings and performance benefits may be gained from using composite materials… …composites. Attempts have been made at using thermoplastics as matrix materials but in early years… …the application of the materials were limited by factors such as low elastic modulus, low… 

Page 1 Page 2 Page 3 Page 4 Page 5 Page 6 Page 7

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Van der Westhuizen, A. O. (2013). Impact response of a continuous fibre reinforced thermoplastic from a soft bodied projectile. (Masters Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/80095

Chicago Manual of Style (16th Edition):

Van der Westhuizen, Artho Otto. “Impact response of a continuous fibre reinforced thermoplastic from a soft bodied projectile.” 2013. Masters Thesis, Stellenbosch University. Accessed May 20, 2019. http://hdl.handle.net/10019.1/80095.

MLA Handbook (7th Edition):

Van der Westhuizen, Artho Otto. “Impact response of a continuous fibre reinforced thermoplastic from a soft bodied projectile.” 2013. Web. 20 May 2019.

Vancouver:

Van der Westhuizen AO. Impact response of a continuous fibre reinforced thermoplastic from a soft bodied projectile. [Internet] [Masters thesis]. Stellenbosch University; 2013. [cited 2019 May 20]. Available from: http://hdl.handle.net/10019.1/80095.

Council of Science Editors:

Van der Westhuizen AO. Impact response of a continuous fibre reinforced thermoplastic from a soft bodied projectile. [Masters Thesis]. Stellenbosch University; 2013. Available from: http://hdl.handle.net/10019.1/80095


University of Dayton

26. Borth, David J. Non-Destructive Evaluation of Urethane-Ester Coating Systems Using the Scanning Kelvin Probe Technique.

Degree: MS(M.S.), Materials Engineering, 2018, University of Dayton

 The research described herein examines the effect of hydrolytic decomposition on the work function of polyurethane rain erosion coatings (REC). Two groups of panels, one… (more)

Subjects/Keywords: Materials Science; Aerospace Materials; Polymer Chemistry; Non-destructive Analysis; Scanning Kelvin Probe; SKP; Polyurethane; Hydrolysis; Work Function; Thermomechanical Analysis; TMA; Attenuated Total Reflectance Fourier-transform Infrared Spectroscopy; FT-IR; Raman; Aircraft Coatings

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Borth, D. J. (2018). Non-Destructive Evaluation of Urethane-Ester Coating Systems Using the Scanning Kelvin Probe Technique. (Masters Thesis). University of Dayton. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=dayton1524749968517527

Chicago Manual of Style (16th Edition):

Borth, David J. “Non-Destructive Evaluation of Urethane-Ester Coating Systems Using the Scanning Kelvin Probe Technique.” 2018. Masters Thesis, University of Dayton. Accessed May 20, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1524749968517527.

MLA Handbook (7th Edition):

Borth, David J. “Non-Destructive Evaluation of Urethane-Ester Coating Systems Using the Scanning Kelvin Probe Technique.” 2018. Web. 20 May 2019.

Vancouver:

Borth DJ. Non-Destructive Evaluation of Urethane-Ester Coating Systems Using the Scanning Kelvin Probe Technique. [Internet] [Masters thesis]. University of Dayton; 2018. [cited 2019 May 20]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1524749968517527.

Council of Science Editors:

Borth DJ. Non-Destructive Evaluation of Urethane-Ester Coating Systems Using the Scanning Kelvin Probe Technique. [Masters Thesis]. University of Dayton; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1524749968517527

27. Soltis, Jared T. Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades.

Degree: MS, Aerospace Engineering, 2013, Penn State University

 The goal of this research was to design a helicopter rotor blade lead edge that had high sand erosion resistance and was conducive to ultrasonic… (more)

Subjects/Keywords: aircraft icing; de-icing systems; ice adhesion strength; ultrasonic de-icing; erosion resistant materials

…91 5.1.2. Ice Adhesion Strength of Erosion Resistant Materials… …7 Figure 8: Comparison of adhesion strength for potential leading edge materials (16… …materials. Since I have little knowledge in the world of material science and coatings, Dr. Wolfe… …thereon. xv 1. Introduction 1.1. Icing Overview 1.1.1. Aircraft Ice Testing History… …Aircraft icing was not a concern for early aviators, mainly because the lack of technical… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Soltis, J. T. (2013). Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/19062

Chicago Manual of Style (16th Edition):

Soltis, Jared T. “Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades.” 2013. Masters Thesis, Penn State University. Accessed May 20, 2019. https://etda.libraries.psu.edu/catalog/19062.

MLA Handbook (7th Edition):

Soltis, Jared T. “Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades.” 2013. Web. 20 May 2019.

Vancouver:

Soltis JT. Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades. [Internet] [Masters thesis]. Penn State University; 2013. [cited 2019 May 20]. Available from: https://etda.libraries.psu.edu/catalog/19062.

Council of Science Editors:

Soltis JT. Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades. [Masters Thesis]. Penn State University; 2013. Available from: https://etda.libraries.psu.edu/catalog/19062


Virginia Tech

28. Idrisi, Kamal. Heterogeneous (HG) Blankets for Improved Aircraft Interior Noise Reduction.

Degree: PhD, Mechanical Engineering, 2008, Virginia Tech

 This study involves the modeling and optimization of heterogeneous (HG) blankets for improved reduction of the sound transmission through double-panel systems at low frequencies. HG… (more)

Subjects/Keywords: heterogeneous (HG) blankets; vibration-damping materials and structures; sound isolating elements; aircraft interior noise; impedance and mobility method

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Idrisi, K. (2008). Heterogeneous (HG) Blankets for Improved Aircraft Interior Noise Reduction. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/29678

Chicago Manual of Style (16th Edition):

Idrisi, Kamal. “Heterogeneous (HG) Blankets for Improved Aircraft Interior Noise Reduction.” 2008. Doctoral Dissertation, Virginia Tech. Accessed May 20, 2019. http://hdl.handle.net/10919/29678.

MLA Handbook (7th Edition):

Idrisi, Kamal. “Heterogeneous (HG) Blankets for Improved Aircraft Interior Noise Reduction.” 2008. Web. 20 May 2019.

Vancouver:

Idrisi K. Heterogeneous (HG) Blankets for Improved Aircraft Interior Noise Reduction. [Internet] [Doctoral dissertation]. Virginia Tech; 2008. [cited 2019 May 20]. Available from: http://hdl.handle.net/10919/29678.

Council of Science Editors:

Idrisi K. Heterogeneous (HG) Blankets for Improved Aircraft Interior Noise Reduction. [Doctoral Dissertation]. Virginia Tech; 2008. Available from: http://hdl.handle.net/10919/29678

29. Britt, Vicki Owen. Assessment of Preliminary Design Approaches for Metallic Stiffened Cylindrical Shell Instability Problems.

Degree: PhD, Aerospace Engineering, 2007, Old Dominion University

  A preliminary design tool for metallic stiffened fuselage cylindrical panels subjected to longitudinal compression has been developed and validated by comparison to test results.… (more)

Subjects/Keywords: Aircraft; Cylindrical shell; Fuselages; Metallic panels; Navigation, Guidance, Control and Dynamics; Structures and Materials; Systems Engineering and Multidisciplinary Design Optimization

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Britt, V. O. (2007). Assessment of Preliminary Design Approaches for Metallic Stiffened Cylindrical Shell Instability Problems. (Doctoral Dissertation). Old Dominion University. Retrieved from 9780549122470 ; https://digitalcommons.odu.edu/mae_etds/48

Chicago Manual of Style (16th Edition):

Britt, Vicki Owen. “Assessment of Preliminary Design Approaches for Metallic Stiffened Cylindrical Shell Instability Problems.” 2007. Doctoral Dissertation, Old Dominion University. Accessed May 20, 2019. 9780549122470 ; https://digitalcommons.odu.edu/mae_etds/48.

MLA Handbook (7th Edition):

Britt, Vicki Owen. “Assessment of Preliminary Design Approaches for Metallic Stiffened Cylindrical Shell Instability Problems.” 2007. Web. 20 May 2019.

Vancouver:

Britt VO. Assessment of Preliminary Design Approaches for Metallic Stiffened Cylindrical Shell Instability Problems. [Internet] [Doctoral dissertation]. Old Dominion University; 2007. [cited 2019 May 20]. Available from: 9780549122470 ; https://digitalcommons.odu.edu/mae_etds/48.

Council of Science Editors:

Britt VO. Assessment of Preliminary Design Approaches for Metallic Stiffened Cylindrical Shell Instability Problems. [Doctoral Dissertation]. Old Dominion University; 2007. Available from: 9780549122470 ; https://digitalcommons.odu.edu/mae_etds/48

30. Gamble, Lawren. Bioinspired Control of Rudderless Morphing UAVs.

Degree: PhD, Aerospace Engineering, 2018, University of Michigan

 Morphing to seamlessly alter aircraft geometry for either multi-mission or adaptive fly-by-feel flight has recently become an emerging field of research. With the added benefits… (more)

Subjects/Keywords: morphing; rudderless aircraft; smart materials; wind tunnel; bioinspiration; aerodynamics; Aerospace Engineering; Engineering

…morphing concept and proposed configurations for a rudderless aircraft from [75] Search… …results of yearly publications containing both ’morphing’ and ’aircraft’, generated with Google… …Demonstration of the bioinspired aircraft with left actuator deflected where θ represents the fiber… …geometry of the rudderless aircraft consistent with prior studies on tail effects [33]… …x28;a) Schematic of experimental setup (b) mounted aircraft in wind tunnel… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Gamble, L. (2018). Bioinspired Control of Rudderless Morphing UAVs. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/145843

Chicago Manual of Style (16th Edition):

Gamble, Lawren. “Bioinspired Control of Rudderless Morphing UAVs.” 2018. Doctoral Dissertation, University of Michigan. Accessed May 20, 2019. http://hdl.handle.net/2027.42/145843.

MLA Handbook (7th Edition):

Gamble, Lawren. “Bioinspired Control of Rudderless Morphing UAVs.” 2018. Web. 20 May 2019.

Vancouver:

Gamble L. Bioinspired Control of Rudderless Morphing UAVs. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2019 May 20]. Available from: http://hdl.handle.net/2027.42/145843.

Council of Science Editors:

Gamble L. Bioinspired Control of Rudderless Morphing UAVs. [Doctoral Dissertation]. University of Michigan; 2018. Available from: http://hdl.handle.net/2027.42/145843

[1] [2]

.