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You searched for subject:(Aerodynamic). Showing records 1 – 30 of 513 total matches.

[1] [2] [3] [4] [5] … [18]

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Anna University

1. Selvi rajan S. Investigations into aerodynamics Of bridges through wind tunnel testing;.

Degree: Investigations into aerodynamics Of bridges through wind tunnel testing, 2015, Anna University

Aerodynamic studies on cable stayed bridge deck model based on newlineexperimental approach have been examined in the present investigation The newlinemost elementary tool available for… (more)

Subjects/Keywords: Aerodynamic; Aluminium strips

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APA (6th Edition):

S, S. r. (2015). Investigations into aerodynamics Of bridges through wind tunnel testing;. (Thesis). Anna University. Retrieved from http://shodhganga.inflibnet.ac.in/handle/10603/44196

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):

S, Selvi rajan. “Investigations into aerodynamics Of bridges through wind tunnel testing;.” 2015. Thesis, Anna University. Accessed April 23, 2019. http://shodhganga.inflibnet.ac.in/handle/10603/44196.

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

MLA Handbook (7th Edition):

S, Selvi rajan. “Investigations into aerodynamics Of bridges through wind tunnel testing;.” 2015. Web. 23 Apr 2019.

Vancouver:

S Sr. Investigations into aerodynamics Of bridges through wind tunnel testing;. [Internet] [Thesis]. Anna University; 2015. [cited 2019 Apr 23]. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/44196.

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

Council of Science Editors:

S Sr. Investigations into aerodynamics Of bridges through wind tunnel testing;. [Thesis]. Anna University; 2015. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/44196

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


Addis Ababa University

2. Tamiru, Bayissa. RADON PROGENY DEPOSITION IN RESPIRATORY TRACT: COMPARATIVE ANALYSIS OF MODELS .

Degree: 2012, Addis Ababa University

 Cheng (2003) model of the extra-thoracic respiratory tract was used to calculate the deposition efficiency of aerosols of aerodynamic diameter ranging from 0.1 m to… (more)

Subjects/Keywords: aerosols; aerodynamic diameter

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APA (6th Edition):

Tamiru, B. (2012). RADON PROGENY DEPOSITION IN RESPIRATORY TRACT: COMPARATIVE ANALYSIS OF MODELS . (Thesis). Addis Ababa University. Retrieved from http://etd.aau.edu.et/dspace/handle/123456789/1187

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):

Tamiru, Bayissa. “RADON PROGENY DEPOSITION IN RESPIRATORY TRACT: COMPARATIVE ANALYSIS OF MODELS .” 2012. Thesis, Addis Ababa University. Accessed April 23, 2019. http://etd.aau.edu.et/dspace/handle/123456789/1187.

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

MLA Handbook (7th Edition):

Tamiru, Bayissa. “RADON PROGENY DEPOSITION IN RESPIRATORY TRACT: COMPARATIVE ANALYSIS OF MODELS .” 2012. Web. 23 Apr 2019.

Vancouver:

Tamiru B. RADON PROGENY DEPOSITION IN RESPIRATORY TRACT: COMPARATIVE ANALYSIS OF MODELS . [Internet] [Thesis]. Addis Ababa University; 2012. [cited 2019 Apr 23]. Available from: http://etd.aau.edu.et/dspace/handle/123456789/1187.

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

Council of Science Editors:

Tamiru B. RADON PROGENY DEPOSITION IN RESPIRATORY TRACT: COMPARATIVE ANALYSIS OF MODELS . [Thesis]. Addis Ababa University; 2012. Available from: http://etd.aau.edu.et/dspace/handle/123456789/1187

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


Miami University

3. McCarthy, Meghan K. FACTORS AFFECTING AERODYNAMIC MEASUREMENT IN PEDIATRIC AIRWAY PATHOLOGIES.

Degree: MA, Speech Pathology and Audiology, 2007, Miami University

 This study was a retrospective chart review designed to evaluate factors that impact the collection of aerodynamic data in pediatric airway patients. The study included… (more)

Subjects/Keywords: AERODYNAMIC; aerodynamic protocol; Vocal fold; Vocal; perform an aerodynamic; perform an aerodynamic protocol; phonation

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APA (6th Edition):

McCarthy, M. K. (2007). FACTORS AFFECTING AERODYNAMIC MEASUREMENT IN PEDIATRIC AIRWAY PATHOLOGIES. (Masters Thesis). Miami University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=miami1177036003

Chicago Manual of Style (16th Edition):

McCarthy, Meghan K. “FACTORS AFFECTING AERODYNAMIC MEASUREMENT IN PEDIATRIC AIRWAY PATHOLOGIES.” 2007. Masters Thesis, Miami University. Accessed April 23, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=miami1177036003.

MLA Handbook (7th Edition):

McCarthy, Meghan K. “FACTORS AFFECTING AERODYNAMIC MEASUREMENT IN PEDIATRIC AIRWAY PATHOLOGIES.” 2007. Web. 23 Apr 2019.

Vancouver:

McCarthy MK. FACTORS AFFECTING AERODYNAMIC MEASUREMENT IN PEDIATRIC AIRWAY PATHOLOGIES. [Internet] [Masters thesis]. Miami University; 2007. [cited 2019 Apr 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=miami1177036003.

Council of Science Editors:

McCarthy MK. FACTORS AFFECTING AERODYNAMIC MEASUREMENT IN PEDIATRIC AIRWAY PATHOLOGIES. [Masters Thesis]. Miami University; 2007. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=miami1177036003


Anna University

4. Bruce ralphin rose J. Experimental investigation and Analysis on aeroelastic performance For aileron reversal and gust Response of a transport aircraft;.

Degree: Experimental investigation and Analysis on aeroelastic performance For aileron reversal and gust Response of a transport aircraft, 2015, Anna University

At high cruising speeds airplane wing structures shall experience newlineair loads of significant magnitudes from various directions The flexible wing newlinestructure with an elevated aspect… (more)

Subjects/Keywords: Aerodynamic Quantities; Aeroelastic Control Reversal

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APA (6th Edition):

J, B. r. r. (2015). Experimental investigation and Analysis on aeroelastic performance For aileron reversal and gust Response of a transport aircraft;. (Thesis). Anna University. Retrieved from http://shodhganga.inflibnet.ac.in/handle/10603/39432

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):

J, Bruce ralphin rose. “Experimental investigation and Analysis on aeroelastic performance For aileron reversal and gust Response of a transport aircraft;.” 2015. Thesis, Anna University. Accessed April 23, 2019. http://shodhganga.inflibnet.ac.in/handle/10603/39432.

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

MLA Handbook (7th Edition):

J, Bruce ralphin rose. “Experimental investigation and Analysis on aeroelastic performance For aileron reversal and gust Response of a transport aircraft;.” 2015. Web. 23 Apr 2019.

Vancouver:

J Brr. Experimental investigation and Analysis on aeroelastic performance For aileron reversal and gust Response of a transport aircraft;. [Internet] [Thesis]. Anna University; 2015. [cited 2019 Apr 23]. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/39432.

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

Council of Science Editors:

J Brr. Experimental investigation and Analysis on aeroelastic performance For aileron reversal and gust Response of a transport aircraft;. [Thesis]. Anna University; 2015. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/39432

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


Penn State University

5. Frymire, Stephen Paul. THE DEVELOPMENT OF A SECURITY-SCREENING PORTAL FOR HUMAN AERODYNAMIC WAKE SAMPLING.

Degree: MS, Mechanical Engineering, 2009, Penn State University

 In an effort to increase the throughput of explosive trace sampling in airport security, a trace sampling portal was designed based upon the recirculation region… (more)

Subjects/Keywords: Trace Collection; Aerodynamic Sampling; Impactor

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APA (6th Edition):

Frymire, S. P. (2009). THE DEVELOPMENT OF A SECURITY-SCREENING PORTAL FOR HUMAN AERODYNAMIC WAKE SAMPLING. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/9985

Chicago Manual of Style (16th Edition):

Frymire, Stephen Paul. “THE DEVELOPMENT OF A SECURITY-SCREENING PORTAL FOR HUMAN AERODYNAMIC WAKE SAMPLING.” 2009. Masters Thesis, Penn State University. Accessed April 23, 2019. https://etda.libraries.psu.edu/catalog/9985.

MLA Handbook (7th Edition):

Frymire, Stephen Paul. “THE DEVELOPMENT OF A SECURITY-SCREENING PORTAL FOR HUMAN AERODYNAMIC WAKE SAMPLING.” 2009. Web. 23 Apr 2019.

Vancouver:

Frymire SP. THE DEVELOPMENT OF A SECURITY-SCREENING PORTAL FOR HUMAN AERODYNAMIC WAKE SAMPLING. [Internet] [Masters thesis]. Penn State University; 2009. [cited 2019 Apr 23]. Available from: https://etda.libraries.psu.edu/catalog/9985.

Council of Science Editors:

Frymire SP. THE DEVELOPMENT OF A SECURITY-SCREENING PORTAL FOR HUMAN AERODYNAMIC WAKE SAMPLING. [Masters Thesis]. Penn State University; 2009. Available from: https://etda.libraries.psu.edu/catalog/9985


Ryerson University

6. Yokota, Jeffrey. Computational aero acounstics analysis of an aircraft climate control system.

Degree: 2009, Ryerson University

 With a higher standard of living and education, engineers are paying more attention on how the surrounding environment affects the public's comfort. Aircraft cabin noise… (more)

Subjects/Keywords: Airplanes  – Noise  – Measurement.; Aerodynamic noise.

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APA (6th Edition):

Yokota, J. (2009). Computational aero acounstics analysis of an aircraft climate control system. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A6718

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):

Yokota, Jeffrey. “Computational aero acounstics analysis of an aircraft climate control system.” 2009. Thesis, Ryerson University. Accessed April 23, 2019. https://digital.library.ryerson.ca/islandora/object/RULA%3A6718.

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

MLA Handbook (7th Edition):

Yokota, Jeffrey. “Computational aero acounstics analysis of an aircraft climate control system.” 2009. Web. 23 Apr 2019.

Vancouver:

Yokota J. Computational aero acounstics analysis of an aircraft climate control system. [Internet] [Thesis]. Ryerson University; 2009. [cited 2019 Apr 23]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6718.

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

Council of Science Editors:

Yokota J. Computational aero acounstics analysis of an aircraft climate control system. [Thesis]. Ryerson University; 2009. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6718

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


University of Minnesota

7. Qi, Lejun. Aerosol printing of colloidal nanocrystals by aerodynamic focusing.

Degree: PhD, Material Science and Engineering, 2010, University of Minnesota

 Colloidal synthesized semiconductor nanocrystals, or quantum dots, have shown promise as the active material in electronic and optoelectronic applications, because of their high quantum yield,… (more)

Subjects/Keywords: Aerodynamic focusing; Aerosol; Colloids; Nanocrystal

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APA (6th Edition):

Qi, L. (2010). Aerosol printing of colloidal nanocrystals by aerodynamic focusing. (Doctoral Dissertation). University of Minnesota. Retrieved from http://purl.umn.edu/95491

Chicago Manual of Style (16th Edition):

Qi, Lejun. “Aerosol printing of colloidal nanocrystals by aerodynamic focusing.” 2010. Doctoral Dissertation, University of Minnesota. Accessed April 23, 2019. http://purl.umn.edu/95491.

MLA Handbook (7th Edition):

Qi, Lejun. “Aerosol printing of colloidal nanocrystals by aerodynamic focusing.” 2010. Web. 23 Apr 2019.

Vancouver:

Qi L. Aerosol printing of colloidal nanocrystals by aerodynamic focusing. [Internet] [Doctoral dissertation]. University of Minnesota; 2010. [cited 2019 Apr 23]. Available from: http://purl.umn.edu/95491.

Council of Science Editors:

Qi L. Aerosol printing of colloidal nanocrystals by aerodynamic focusing. [Doctoral Dissertation]. University of Minnesota; 2010. Available from: http://purl.umn.edu/95491


University of Toronto

8. Telidetzki, Karla. Application of Jetstream to a Suite of Aerodynamic Shape Optimization Problems.

Degree: 2014, University of Toronto

The impact of dimensionality on three aerodynamic optimization cases is studied to determine the effect of the number of geometric design variables. The cases investigated… (more)

Subjects/Keywords: Aerodynamic design; Aerodynamic shape optimization; Computational fluid dynamics; Geometry parameterization; 0538

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APA (6th Edition):

Telidetzki, K. (2014). Application of Jetstream to a Suite of Aerodynamic Shape Optimization Problems. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/67967

Chicago Manual of Style (16th Edition):

Telidetzki, Karla. “Application of Jetstream to a Suite of Aerodynamic Shape Optimization Problems.” 2014. Masters Thesis, University of Toronto. Accessed April 23, 2019. http://hdl.handle.net/1807/67967.

MLA Handbook (7th Edition):

Telidetzki, Karla. “Application of Jetstream to a Suite of Aerodynamic Shape Optimization Problems.” 2014. Web. 23 Apr 2019.

Vancouver:

Telidetzki K. Application of Jetstream to a Suite of Aerodynamic Shape Optimization Problems. [Internet] [Masters thesis]. University of Toronto; 2014. [cited 2019 Apr 23]. Available from: http://hdl.handle.net/1807/67967.

Council of Science Editors:

Telidetzki K. Application of Jetstream to a Suite of Aerodynamic Shape Optimization Problems. [Masters Thesis]. University of Toronto; 2014. Available from: http://hdl.handle.net/1807/67967


Anna University

9. Mukesh R. Application of non traditional Optimisation technique and kriging Methodology based surrogate model For airfoil design optimisation;.

Degree: Application of non traditional Optimisation technique and kriging Methodology based surrogate model For airfoil design optimisation, 2015, Anna University

Nowadays engineering analysis relies heavily on computer based newlinesolution algorithms to investigate the performance of an engineering system newlineComputational fluid dynamics CFD is one of… (more)

Subjects/Keywords: Aerodynamic shape optimisation; Computational fluid dynamics

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APA (6th Edition):

R, M. (2015). Application of non traditional Optimisation technique and kriging Methodology based surrogate model For airfoil design optimisation;. (Thesis). Anna University. Retrieved from http://shodhganga.inflibnet.ac.in/handle/10603/54553

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):

R, Mukesh. “Application of non traditional Optimisation technique and kriging Methodology based surrogate model For airfoil design optimisation;.” 2015. Thesis, Anna University. Accessed April 23, 2019. http://shodhganga.inflibnet.ac.in/handle/10603/54553.

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

MLA Handbook (7th Edition):

R, Mukesh. “Application of non traditional Optimisation technique and kriging Methodology based surrogate model For airfoil design optimisation;.” 2015. Web. 23 Apr 2019.

Vancouver:

R M. Application of non traditional Optimisation technique and kriging Methodology based surrogate model For airfoil design optimisation;. [Internet] [Thesis]. Anna University; 2015. [cited 2019 Apr 23]. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/54553.

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

Council of Science Editors:

R M. Application of non traditional Optimisation technique and kriging Methodology based surrogate model For airfoil design optimisation;. [Thesis]. Anna University; 2015. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/54553

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

10. Sarmast, Sasan. Numerical Simulation of the Flow around the Wheel within Wheelhouse.

Degree: 2010, Chalmers University of Technology

 Increasing crude oil price and different legislation for vehicle emissions forced the vehicle manufacturer to produce more efficient vehicles. Road vehicle aerodynamics reaches its limits,… (more)

Subjects/Keywords: LES; large eddy simulations; vehicle aerodynamic

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APA (6th Edition):

Sarmast, S. (2010). Numerical Simulation of the Flow around the Wheel within Wheelhouse. (Thesis). Chalmers University of Technology. Retrieved from http://studentarbeten.chalmers.se/publication/134955-numerical-simulation-of-the-flow-around-the-wheel-within-wheelhouse

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):

Sarmast, Sasan. “Numerical Simulation of the Flow around the Wheel within Wheelhouse.” 2010. Thesis, Chalmers University of Technology. Accessed April 23, 2019. http://studentarbeten.chalmers.se/publication/134955-numerical-simulation-of-the-flow-around-the-wheel-within-wheelhouse.

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

MLA Handbook (7th Edition):

Sarmast, Sasan. “Numerical Simulation of the Flow around the Wheel within Wheelhouse.” 2010. Web. 23 Apr 2019.

Vancouver:

Sarmast S. Numerical Simulation of the Flow around the Wheel within Wheelhouse. [Internet] [Thesis]. Chalmers University of Technology; 2010. [cited 2019 Apr 23]. Available from: http://studentarbeten.chalmers.se/publication/134955-numerical-simulation-of-the-flow-around-the-wheel-within-wheelhouse.

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

Council of Science Editors:

Sarmast S. Numerical Simulation of the Flow around the Wheel within Wheelhouse. [Thesis]. Chalmers University of Technology; 2010. Available from: http://studentarbeten.chalmers.se/publication/134955-numerical-simulation-of-the-flow-around-the-wheel-within-wheelhouse

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


University of Ontario Institute of Technology

11. Abdel-Rahman, Abdalla. Development and application of an integrated aerodynamic and thermodynamic testing system for cars.

Degree: 2015, University of Ontario Institute of Technology

 In this thesis an integrated aerodynamic and thermodynamic testing system was developed. It consists of an incremental force measuring system (FMS) that was designed and… (more)

Subjects/Keywords: Aerodynamic; Thermodynamic; Aero-thermal; Cars; Improvement

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APA (6th Edition):

Abdel-Rahman, A. (2015). Development and application of an integrated aerodynamic and thermodynamic testing system for cars. (Thesis). University of Ontario Institute of Technology. Retrieved from http://hdl.handle.net/10155/896

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):

Abdel-Rahman, Abdalla. “Development and application of an integrated aerodynamic and thermodynamic testing system for cars.” 2015. Thesis, University of Ontario Institute of Technology. Accessed April 23, 2019. http://hdl.handle.net/10155/896.

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

MLA Handbook (7th Edition):

Abdel-Rahman, Abdalla. “Development and application of an integrated aerodynamic and thermodynamic testing system for cars.” 2015. Web. 23 Apr 2019.

Vancouver:

Abdel-Rahman A. Development and application of an integrated aerodynamic and thermodynamic testing system for cars. [Internet] [Thesis]. University of Ontario Institute of Technology; 2015. [cited 2019 Apr 23]. Available from: http://hdl.handle.net/10155/896.

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

Council of Science Editors:

Abdel-Rahman A. Development and application of an integrated aerodynamic and thermodynamic testing system for cars. [Thesis]. University of Ontario Institute of Technology; 2015. Available from: http://hdl.handle.net/10155/896

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


Loughborough University

12. Malik, Abdullah. Suppression of junction flow effects in half model wind tunnel testing.

Degree: PhD, 2013, Loughborough University

 Half model testing is considered a valuable wind tunnel technique that offers many benefits over conventional full span testing. The technique suffers from aerodynamic losses… (more)

Subjects/Keywords: Localised suction; Aerodynamic losses; Horseshoe vortex

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APA (6th Edition):

Malik, A. (2013). Suppression of junction flow effects in half model wind tunnel testing. (Doctoral Dissertation). Loughborough University. Retrieved from https://dspace.lboro.ac.uk/2134/11568 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.566517

Chicago Manual of Style (16th Edition):

Malik, Abdullah. “Suppression of junction flow effects in half model wind tunnel testing.” 2013. Doctoral Dissertation, Loughborough University. Accessed April 23, 2019. https://dspace.lboro.ac.uk/2134/11568 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.566517.

MLA Handbook (7th Edition):

Malik, Abdullah. “Suppression of junction flow effects in half model wind tunnel testing.” 2013. Web. 23 Apr 2019.

Vancouver:

Malik A. Suppression of junction flow effects in half model wind tunnel testing. [Internet] [Doctoral dissertation]. Loughborough University; 2013. [cited 2019 Apr 23]. Available from: https://dspace.lboro.ac.uk/2134/11568 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.566517.

Council of Science Editors:

Malik A. Suppression of junction flow effects in half model wind tunnel testing. [Doctoral Dissertation]. Loughborough University; 2013. Available from: https://dspace.lboro.ac.uk/2134/11568 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.566517

13. Saravanan P. Aerodynamic analysis of small horizontal axis wind turbine blades with winglets;.

Degree: Aerodynamic analysis of small horizontal axis wind turbine blades, 2014, Anna University

The aerodynamic characteristics of winglet added with small wind newlineturbine rotor blades are focused in this research work. The experiments and newlinecomputational studies are carried… (more)

Subjects/Keywords: Aerodynamic; Mechanical Engineerings; Wind turbine blades; Winglets

Page 1

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APA (6th Edition):

P, S. (2014). Aerodynamic analysis of small horizontal axis wind turbine blades with winglets;. (Thesis). Anna University. Retrieved from http://shodhganga.inflibnet.ac.in/handle/10603/17549

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):

P, Saravanan. “Aerodynamic analysis of small horizontal axis wind turbine blades with winglets;.” 2014. Thesis, Anna University. Accessed April 23, 2019. http://shodhganga.inflibnet.ac.in/handle/10603/17549.

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

MLA Handbook (7th Edition):

P, Saravanan. “Aerodynamic analysis of small horizontal axis wind turbine blades with winglets;.” 2014. Web. 23 Apr 2019.

Vancouver:

P S. Aerodynamic analysis of small horizontal axis wind turbine blades with winglets;. [Internet] [Thesis]. Anna University; 2014. [cited 2019 Apr 23]. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/17549.

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

Council of Science Editors:

P S. Aerodynamic analysis of small horizontal axis wind turbine blades with winglets;. [Thesis]. Anna University; 2014. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/17549

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


University of Canterbury

14. Mautner, Helene. A Cross-System Instrumental Voice Profile of the Aging Voice: With Considerations of Jaw Posture Effects.

Degree: Communication Disorders, 2011, University of Canterbury

 Purpose: An open mouth approach is used in voice therapy for enhancing speech and voice production and relaxing the laryngeal musculature. The acoustic and physiological… (more)

Subjects/Keywords: Voice; Aging; Jaw Posture; Acoustic; Aerodynamic; Geriatric

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APA (6th Edition):

Mautner, H. (2011). A Cross-System Instrumental Voice Profile of the Aging Voice: With Considerations of Jaw Posture Effects. (Thesis). University of Canterbury. Retrieved from http://hdl.handle.net/10092/5183

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):

Mautner, Helene. “A Cross-System Instrumental Voice Profile of the Aging Voice: With Considerations of Jaw Posture Effects.” 2011. Thesis, University of Canterbury. Accessed April 23, 2019. http://hdl.handle.net/10092/5183.

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

MLA Handbook (7th Edition):

Mautner, Helene. “A Cross-System Instrumental Voice Profile of the Aging Voice: With Considerations of Jaw Posture Effects.” 2011. Web. 23 Apr 2019.

Vancouver:

Mautner H. A Cross-System Instrumental Voice Profile of the Aging Voice: With Considerations of Jaw Posture Effects. [Internet] [Thesis]. University of Canterbury; 2011. [cited 2019 Apr 23]. Available from: http://hdl.handle.net/10092/5183.

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

Council of Science Editors:

Mautner H. A Cross-System Instrumental Voice Profile of the Aging Voice: With Considerations of Jaw Posture Effects. [Thesis]. University of Canterbury; 2011. Available from: http://hdl.handle.net/10092/5183

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


University of Virginia

15. Green, Justin. Morphing Hypersonic Inflatable Aerodynamic Decelerator.

Degree: MS, Mechanical and Aerospace Engineering, 2012, University of Virginia

 The ever growing complexity of missions to planetary bodies has pushed the Viking era rigid aeroshell designs to their operational limits. Plans for future robotic… (more)

Subjects/Keywords: HIAD; Hypersonic Infaltable Aerodynamic Decelerator; Morphing; Model

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APA (6th Edition):

Green, J. (2012). Morphing Hypersonic Inflatable Aerodynamic Decelerator. (Doctoral Dissertation). University of Virginia. Retrieved from http://libra.virginia.edu/catalog/libra-oa:2617

Chicago Manual of Style (16th Edition):

Green, Justin. “Morphing Hypersonic Inflatable Aerodynamic Decelerator.” 2012. Doctoral Dissertation, University of Virginia. Accessed April 23, 2019. http://libra.virginia.edu/catalog/libra-oa:2617.

MLA Handbook (7th Edition):

Green, Justin. “Morphing Hypersonic Inflatable Aerodynamic Decelerator.” 2012. Web. 23 Apr 2019.

Vancouver:

Green J. Morphing Hypersonic Inflatable Aerodynamic Decelerator. [Internet] [Doctoral dissertation]. University of Virginia; 2012. [cited 2019 Apr 23]. Available from: http://libra.virginia.edu/catalog/libra-oa:2617.

Council of Science Editors:

Green J. Morphing Hypersonic Inflatable Aerodynamic Decelerator. [Doctoral Dissertation]. University of Virginia; 2012. Available from: http://libra.virginia.edu/catalog/libra-oa:2617


Utah State University

16. Pope, Orrin Dean. Aerodynamic Centers of Arbitrary Airfoils.

Degree: MS, Mechanical and Aerospace Engineering, 2017, Utah State University

  The study of designing stable aircraft has been widespread and ongoing since the early days of Orville and Wilbur Wright and their famous Wright… (more)

Subjects/Keywords: Aerodynamics; airfoil; aerodynamic center; Mechanical Engineering

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APA (6th Edition):

Pope, O. D. (2017). Aerodynamic Centers of Arbitrary Airfoils. (Masters Thesis). Utah State University. Retrieved from https://digitalcommons.usu.edu/etd/6890

Chicago Manual of Style (16th Edition):

Pope, Orrin Dean. “Aerodynamic Centers of Arbitrary Airfoils.” 2017. Masters Thesis, Utah State University. Accessed April 23, 2019. https://digitalcommons.usu.edu/etd/6890.

MLA Handbook (7th Edition):

Pope, Orrin Dean. “Aerodynamic Centers of Arbitrary Airfoils.” 2017. Web. 23 Apr 2019.

Vancouver:

Pope OD. Aerodynamic Centers of Arbitrary Airfoils. [Internet] [Masters thesis]. Utah State University; 2017. [cited 2019 Apr 23]. Available from: https://digitalcommons.usu.edu/etd/6890.

Council of Science Editors:

Pope OD. Aerodynamic Centers of Arbitrary Airfoils. [Masters Thesis]. Utah State University; 2017. Available from: https://digitalcommons.usu.edu/etd/6890


Utah State University

17. Taylor, Jeffrey D. Methods for the Aerostructural Design and Optimization of Wings with Arbitrary Planform and Payload Distribution.

Degree: MS, Mechanical and Aerospace Engineering, 2018, Utah State University

  The design of an aircraft wing often involves the use of mathematical methods for simultaneous aerodynamic and structural design. The goal of many of… (more)

Subjects/Keywords: Aerodynamic; aerostructural; aeroelastic; optimization; Mechanical Engineering

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APA (6th Edition):

Taylor, J. D. (2018). Methods for the Aerostructural Design and Optimization of Wings with Arbitrary Planform and Payload Distribution. (Masters Thesis). Utah State University. Retrieved from https://digitalcommons.usu.edu/etd/6909

Chicago Manual of Style (16th Edition):

Taylor, Jeffrey D. “Methods for the Aerostructural Design and Optimization of Wings with Arbitrary Planform and Payload Distribution.” 2018. Masters Thesis, Utah State University. Accessed April 23, 2019. https://digitalcommons.usu.edu/etd/6909.

MLA Handbook (7th Edition):

Taylor, Jeffrey D. “Methods for the Aerostructural Design and Optimization of Wings with Arbitrary Planform and Payload Distribution.” 2018. Web. 23 Apr 2019.

Vancouver:

Taylor JD. Methods for the Aerostructural Design and Optimization of Wings with Arbitrary Planform and Payload Distribution. [Internet] [Masters thesis]. Utah State University; 2018. [cited 2019 Apr 23]. Available from: https://digitalcommons.usu.edu/etd/6909.

Council of Science Editors:

Taylor JD. Methods for the Aerostructural Design and Optimization of Wings with Arbitrary Planform and Payload Distribution. [Masters Thesis]. Utah State University; 2018. Available from: https://digitalcommons.usu.edu/etd/6909


University of Toronto

18. Luo, Zhanhong. Lateral Post-stall Aerodynamic Modeling using Flight Test Data.

Degree: 2016, University of Toronto

Loss-of-control resulting from airplane upset is a leading cause of worldwide commercial aircraft accidents. In response, the Federal Aviation Administration requires all U.S. air carrier… (more)

Subjects/Keywords: Aerodynamic; Model; Simulink; Stall Model; 0538

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APA (6th Edition):

Luo, Z. (2016). Lateral Post-stall Aerodynamic Modeling using Flight Test Data. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/77345

Chicago Manual of Style (16th Edition):

Luo, Zhanhong. “Lateral Post-stall Aerodynamic Modeling using Flight Test Data.” 2016. Masters Thesis, University of Toronto. Accessed April 23, 2019. http://hdl.handle.net/1807/77345.

MLA Handbook (7th Edition):

Luo, Zhanhong. “Lateral Post-stall Aerodynamic Modeling using Flight Test Data.” 2016. Web. 23 Apr 2019.

Vancouver:

Luo Z. Lateral Post-stall Aerodynamic Modeling using Flight Test Data. [Internet] [Masters thesis]. University of Toronto; 2016. [cited 2019 Apr 23]. Available from: http://hdl.handle.net/1807/77345.

Council of Science Editors:

Luo Z. Lateral Post-stall Aerodynamic Modeling using Flight Test Data. [Masters Thesis]. University of Toronto; 2016. Available from: http://hdl.handle.net/1807/77345


University of Toronto

19. Curiale, Nathanael J. Morphing Wings: A Study Using High-Fidelity Aerodynamic Shape Optimization.

Degree: 2017, University of Toronto

With the aviation industry under pressure to reduce fuel consumption, morphing wings have the capacity to improve aircraft performance, thereby making a significant contribution to… (more)

Subjects/Keywords: Aerodynamic; Engineering; Morphing Wings; Optimization; 0538

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APA (6th Edition):

Curiale, N. J. (2017). Morphing Wings: A Study Using High-Fidelity Aerodynamic Shape Optimization. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/79050

Chicago Manual of Style (16th Edition):

Curiale, Nathanael J. “Morphing Wings: A Study Using High-Fidelity Aerodynamic Shape Optimization.” 2017. Masters Thesis, University of Toronto. Accessed April 23, 2019. http://hdl.handle.net/1807/79050.

MLA Handbook (7th Edition):

Curiale, Nathanael J. “Morphing Wings: A Study Using High-Fidelity Aerodynamic Shape Optimization.” 2017. Web. 23 Apr 2019.

Vancouver:

Curiale NJ. Morphing Wings: A Study Using High-Fidelity Aerodynamic Shape Optimization. [Internet] [Masters thesis]. University of Toronto; 2017. [cited 2019 Apr 23]. Available from: http://hdl.handle.net/1807/79050.

Council of Science Editors:

Curiale NJ. Morphing Wings: A Study Using High-Fidelity Aerodynamic Shape Optimization. [Masters Thesis]. University of Toronto; 2017. Available from: http://hdl.handle.net/1807/79050


Louisiana State University

20. Iverson, Laura M. Aerodynamic Mitigation of Roof Suction Using Solar Panels.

Degree: MSCE, Civil and Environmental Engineering, 2016, Louisiana State University

 This thesis aims to evaluate the feasibility of solar panels to be used as aerodynamic mitigation devices to reduce roof suction caused by high-speed winds… (more)

Subjects/Keywords: wind engineering; solar panels; aerodynamic mitigation

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APA (6th Edition):

Iverson, L. M. (2016). Aerodynamic Mitigation of Roof Suction Using Solar Panels. (Masters Thesis). Louisiana State University. Retrieved from etd-07042016-220053 ; https://digitalcommons.lsu.edu/gradschool_theses/4205

Chicago Manual of Style (16th Edition):

Iverson, Laura M. “Aerodynamic Mitigation of Roof Suction Using Solar Panels.” 2016. Masters Thesis, Louisiana State University. Accessed April 23, 2019. etd-07042016-220053 ; https://digitalcommons.lsu.edu/gradschool_theses/4205.

MLA Handbook (7th Edition):

Iverson, Laura M. “Aerodynamic Mitigation of Roof Suction Using Solar Panels.” 2016. Web. 23 Apr 2019.

Vancouver:

Iverson LM. Aerodynamic Mitigation of Roof Suction Using Solar Panels. [Internet] [Masters thesis]. Louisiana State University; 2016. [cited 2019 Apr 23]. Available from: etd-07042016-220053 ; https://digitalcommons.lsu.edu/gradschool_theses/4205.

Council of Science Editors:

Iverson LM. Aerodynamic Mitigation of Roof Suction Using Solar Panels. [Masters Thesis]. Louisiana State University; 2016. Available from: etd-07042016-220053 ; https://digitalcommons.lsu.edu/gradschool_theses/4205


Université de Sherbrooke

21. Beauchesne-Martel, Philippe. Numerical analysis of subsonic laminar flow aerothermodynamics in microturbomachinery and development of a design methodology .

Degree: 2009, Université de Sherbrooke

 This thesis presents the numerical and analytical study of the aerodynamic and heat transfer in laminar subsonic cascades along with the development of design guidelines… (more)

Subjects/Keywords: Rankine; Laminar; Compressible; Aerodynamic; Design; MEMS; Turbines

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APA (6th Edition):

Beauchesne-Martel, P. (2009). Numerical analysis of subsonic laminar flow aerothermodynamics in microturbomachinery and development of a design methodology . (Masters Thesis). Université de Sherbrooke. Retrieved from http://savoirs.usherbrooke.ca/handle/11143/1479

Chicago Manual of Style (16th Edition):

Beauchesne-Martel, Philippe. “Numerical analysis of subsonic laminar flow aerothermodynamics in microturbomachinery and development of a design methodology .” 2009. Masters Thesis, Université de Sherbrooke. Accessed April 23, 2019. http://savoirs.usherbrooke.ca/handle/11143/1479.

MLA Handbook (7th Edition):

Beauchesne-Martel, Philippe. “Numerical analysis of subsonic laminar flow aerothermodynamics in microturbomachinery and development of a design methodology .” 2009. Web. 23 Apr 2019.

Vancouver:

Beauchesne-Martel P. Numerical analysis of subsonic laminar flow aerothermodynamics in microturbomachinery and development of a design methodology . [Internet] [Masters thesis]. Université de Sherbrooke; 2009. [cited 2019 Apr 23]. Available from: http://savoirs.usherbrooke.ca/handle/11143/1479.

Council of Science Editors:

Beauchesne-Martel P. Numerical analysis of subsonic laminar flow aerothermodynamics in microturbomachinery and development of a design methodology . [Masters Thesis]. Université de Sherbrooke; 2009. Available from: http://savoirs.usherbrooke.ca/handle/11143/1479


Iowa State University

22. Ning, Zhe. Experimental investigations on the aerodynamic and aeroacoustic characteristics of small UAS propellers.

Degree: 2018, Iowa State University

 Unmanned aerial system (UAS) is a hot topic in both industry and academia fields. As a popular planform, the rotary-wing system gains more attentions. The… (more)

Subjects/Keywords: aeroacoustic; Aerodynamic; experiment; Icing; propeller; UAS; Engineering

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APA (6th Edition):

Ning, Z. (2018). Experimental investigations on the aerodynamic and aeroacoustic characteristics of small UAS propellers. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/16427

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):

Ning, Zhe. “Experimental investigations on the aerodynamic and aeroacoustic characteristics of small UAS propellers.” 2018. Thesis, Iowa State University. Accessed April 23, 2019. https://lib.dr.iastate.edu/etd/16427.

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

MLA Handbook (7th Edition):

Ning, Zhe. “Experimental investigations on the aerodynamic and aeroacoustic characteristics of small UAS propellers.” 2018. Web. 23 Apr 2019.

Vancouver:

Ning Z. Experimental investigations on the aerodynamic and aeroacoustic characteristics of small UAS propellers. [Internet] [Thesis]. Iowa State University; 2018. [cited 2019 Apr 23]. Available from: https://lib.dr.iastate.edu/etd/16427.

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

Council of Science Editors:

Ning Z. Experimental investigations on the aerodynamic and aeroacoustic characteristics of small UAS propellers. [Thesis]. Iowa State University; 2018. Available from: https://lib.dr.iastate.edu/etd/16427

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


Linköping University

23. Pereira, Ramón López. Validation of software for the calculation of aerodynamic coefficients : with a focus on the software package Tornado.

Degree: Fluid and Mechanical Engineering Systems, 2010, Linköping University

Several programs exist today for calculating aerodynamic coefficients that with some simplifications provide fast approximations of the values for a real aircraft. Four different… (more)

Subjects/Keywords: Aerodynamic coefficients; Aerodynamiska koefficienter; TECHNOLOGY; TEKNIKVETENSKAP

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APA (6th Edition):

Pereira, R. L. (2010). Validation of software for the calculation of aerodynamic coefficients : with a focus on the software package Tornado. (Thesis). Linköping University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-57972

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):

Pereira, Ramón López. “Validation of software for the calculation of aerodynamic coefficients : with a focus on the software package Tornado.” 2010. Thesis, Linköping University. Accessed April 23, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-57972.

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

MLA Handbook (7th Edition):

Pereira, Ramón López. “Validation of software for the calculation of aerodynamic coefficients : with a focus on the software package Tornado.” 2010. Web. 23 Apr 2019.

Vancouver:

Pereira RL. Validation of software for the calculation of aerodynamic coefficients : with a focus on the software package Tornado. [Internet] [Thesis]. Linköping University; 2010. [cited 2019 Apr 23]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-57972.

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

Council of Science Editors:

Pereira RL. Validation of software for the calculation of aerodynamic coefficients : with a focus on the software package Tornado. [Thesis]. Linköping University; 2010. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-57972

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


Delft University of Technology

24. Xiomara Herrera Feregrino, X.H.F. Study on aerodynamic imbalance of wind turbine rotors: an investigation of effects due to blade pitch assymetry.:.

Degree: 2015, Delft University of Technology

Subjects/Keywords: rotor aerodynamic imbalance

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APA (6th Edition):

Xiomara Herrera Feregrino, X. H. F. (2015). Study on aerodynamic imbalance of wind turbine rotors: an investigation of effects due to blade pitch assymetry.:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:4c1fee72-e90d-444b-b702-772ebfe41073

Chicago Manual of Style (16th Edition):

Xiomara Herrera Feregrino, X H F. “Study on aerodynamic imbalance of wind turbine rotors: an investigation of effects due to blade pitch assymetry.:.” 2015. Masters Thesis, Delft University of Technology. Accessed April 23, 2019. http://resolver.tudelft.nl/uuid:4c1fee72-e90d-444b-b702-772ebfe41073.

MLA Handbook (7th Edition):

Xiomara Herrera Feregrino, X H F. “Study on aerodynamic imbalance of wind turbine rotors: an investigation of effects due to blade pitch assymetry.:.” 2015. Web. 23 Apr 2019.

Vancouver:

Xiomara Herrera Feregrino XHF. Study on aerodynamic imbalance of wind turbine rotors: an investigation of effects due to blade pitch assymetry.:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Apr 23]. Available from: http://resolver.tudelft.nl/uuid:4c1fee72-e90d-444b-b702-772ebfe41073.

Council of Science Editors:

Xiomara Herrera Feregrino XHF. Study on aerodynamic imbalance of wind turbine rotors: an investigation of effects due to blade pitch assymetry.:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:4c1fee72-e90d-444b-b702-772ebfe41073


University of Toronto

25. Leung, Timothy. A Newton-Krylov Approach to Aerodynamic Shape Optimization in Three Dimensions.

Degree: 2010, University of Toronto

A Newton-Krylov algorithm is presented for aerodynamic shape optimization in three dimensions using the Euler equations. An inexact-Newton method is used in the flow solver,… (more)

Subjects/Keywords: Aerodynamic; Shape; Optimization; Newton-Krylov; 0538

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APA (6th Edition):

Leung, T. (2010). A Newton-Krylov Approach to Aerodynamic Shape Optimization in Three Dimensions. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/24811

Chicago Manual of Style (16th Edition):

Leung, Timothy. “A Newton-Krylov Approach to Aerodynamic Shape Optimization in Three Dimensions.” 2010. Doctoral Dissertation, University of Toronto. Accessed April 23, 2019. http://hdl.handle.net/1807/24811.

MLA Handbook (7th Edition):

Leung, Timothy. “A Newton-Krylov Approach to Aerodynamic Shape Optimization in Three Dimensions.” 2010. Web. 23 Apr 2019.

Vancouver:

Leung T. A Newton-Krylov Approach to Aerodynamic Shape Optimization in Three Dimensions. [Internet] [Doctoral dissertation]. University of Toronto; 2010. [cited 2019 Apr 23]. Available from: http://hdl.handle.net/1807/24811.

Council of Science Editors:

Leung T. A Newton-Krylov Approach to Aerodynamic Shape Optimization in Three Dimensions. [Doctoral Dissertation]. University of Toronto; 2010. Available from: http://hdl.handle.net/1807/24811


University of New South Wales

26. Leylek, Zafer. Global Surrogate Modelling of Gas Turbine Aerodynamic Performance.

Degree: Engineering & Information Technology, 2018, University of New South Wales

 The compressor and turbine aerodynamic performance of a gas turbine engine depends on complex three-dimensional unsteady interactions between static and rotating blades. Each component is… (more)

Subjects/Keywords: Compressor; Turbine; Surrogate modelling; Aerodynamic performance

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APA (6th Edition):

Leylek, Z. (2018). Global Surrogate Modelling of Gas Turbine Aerodynamic Performance. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/60074 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:51324/SOURCE2?view=true

Chicago Manual of Style (16th Edition):

Leylek, Zafer. “Global Surrogate Modelling of Gas Turbine Aerodynamic Performance.” 2018. Doctoral Dissertation, University of New South Wales. Accessed April 23, 2019. http://handle.unsw.edu.au/1959.4/60074 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:51324/SOURCE2?view=true.

MLA Handbook (7th Edition):

Leylek, Zafer. “Global Surrogate Modelling of Gas Turbine Aerodynamic Performance.” 2018. Web. 23 Apr 2019.

Vancouver:

Leylek Z. Global Surrogate Modelling of Gas Turbine Aerodynamic Performance. [Internet] [Doctoral dissertation]. University of New South Wales; 2018. [cited 2019 Apr 23]. Available from: http://handle.unsw.edu.au/1959.4/60074 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:51324/SOURCE2?view=true.

Council of Science Editors:

Leylek Z. Global Surrogate Modelling of Gas Turbine Aerodynamic Performance. [Doctoral Dissertation]. University of New South Wales; 2018. Available from: http://handle.unsw.edu.au/1959.4/60074 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:51324/SOURCE2?view=true


Colorado State University

27. Kamin, David Jeffrey. Exploration of a geometric approach for estimating snow surface roughness.

Degree: MS(M.S.), Ecosystem Science and Sustainability, 2016, Colorado State University

 The roughness of a surface that influences atmospheric turbulence is estimated as the aerodynamic roughness length (Z0), and is used to understand the flow of… (more)

Subjects/Keywords: aerodynamic roughness length; anemometric; geometric; snow

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APA (6th Edition):

Kamin, D. J. (2016). Exploration of a geometric approach for estimating snow surface roughness. (Masters Thesis). Colorado State University. Retrieved from http://hdl.handle.net/10217/170391

Chicago Manual of Style (16th Edition):

Kamin, David Jeffrey. “Exploration of a geometric approach for estimating snow surface roughness.” 2016. Masters Thesis, Colorado State University. Accessed April 23, 2019. http://hdl.handle.net/10217/170391.

MLA Handbook (7th Edition):

Kamin, David Jeffrey. “Exploration of a geometric approach for estimating snow surface roughness.” 2016. Web. 23 Apr 2019.

Vancouver:

Kamin DJ. Exploration of a geometric approach for estimating snow surface roughness. [Internet] [Masters thesis]. Colorado State University; 2016. [cited 2019 Apr 23]. Available from: http://hdl.handle.net/10217/170391.

Council of Science Editors:

Kamin DJ. Exploration of a geometric approach for estimating snow surface roughness. [Masters Thesis]. Colorado State University; 2016. Available from: http://hdl.handle.net/10217/170391

28. Constanzo, Fernão de Melo. Análise teórica e experimental da influência da fuselagem sobre a posição do centro aerodinâmico da asa em condições de baixa velocidade.

Degree: Mestrado, Aeronaves, 2009, University of São Paulo

A influência da fuselagem sobre a posição do centro aerodinâmico da asa é complexa e deve ser considerada nos cálculos de equilíbrio e estabilidade estática… (more)

Subjects/Keywords: Aerodynamic center; Aerodynamic interference; Aeronaves; Aircrafts; Centro aerodinâmico; Fuselage influence; Influência da fuselagem; Interferência aerodinâmica

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APA (6th Edition):

Constanzo, F. d. M. (2009). Análise teórica e experimental da influência da fuselagem sobre a posição do centro aerodinâmico da asa em condições de baixa velocidade. (Masters Thesis). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/18/18148/tde-13012011-154655/ ;

Chicago Manual of Style (16th Edition):

Constanzo, Fernão de Melo. “Análise teórica e experimental da influência da fuselagem sobre a posição do centro aerodinâmico da asa em condições de baixa velocidade.” 2009. Masters Thesis, University of São Paulo. Accessed April 23, 2019. http://www.teses.usp.br/teses/disponiveis/18/18148/tde-13012011-154655/ ;.

MLA Handbook (7th Edition):

Constanzo, Fernão de Melo. “Análise teórica e experimental da influência da fuselagem sobre a posição do centro aerodinâmico da asa em condições de baixa velocidade.” 2009. Web. 23 Apr 2019.

Vancouver:

Constanzo FdM. Análise teórica e experimental da influência da fuselagem sobre a posição do centro aerodinâmico da asa em condições de baixa velocidade. [Internet] [Masters thesis]. University of São Paulo; 2009. [cited 2019 Apr 23]. Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-13012011-154655/ ;.

Council of Science Editors:

Constanzo FdM. Análise teórica e experimental da influência da fuselagem sobre a posição do centro aerodinâmico da asa em condições de baixa velocidade. [Masters Thesis]. University of São Paulo; 2009. Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-13012011-154655/ ;


Miami University

29. May, Shelley Katherine. Repeatability of Aerodynamic Measures in Children, Ages 4.0-5.11 Years.

Degree: MA, Speech Pathology and Audiology, 2010, Miami University

 The purpose of this study was to determine the short-term repeatability of average airflow in children, ages 4.0 – 5.11 years. Thirty participants with healthy… (more)

Subjects/Keywords: Speech Therapy; average airflow; aerodynamic measures; repeatability; children; fundamental frequency; intensity; Phonatory Aerodynamic System

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APA (6th Edition):

May, S. K. (2010). Repeatability of Aerodynamic Measures in Children, Ages 4.0-5.11 Years. (Masters Thesis). Miami University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=miami1272376560

Chicago Manual of Style (16th Edition):

May, Shelley Katherine. “Repeatability of Aerodynamic Measures in Children, Ages 4.0-5.11 Years.” 2010. Masters Thesis, Miami University. Accessed April 23, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=miami1272376560.

MLA Handbook (7th Edition):

May, Shelley Katherine. “Repeatability of Aerodynamic Measures in Children, Ages 4.0-5.11 Years.” 2010. Web. 23 Apr 2019.

Vancouver:

May SK. Repeatability of Aerodynamic Measures in Children, Ages 4.0-5.11 Years. [Internet] [Masters thesis]. Miami University; 2010. [cited 2019 Apr 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=miami1272376560.

Council of Science Editors:

May SK. Repeatability of Aerodynamic Measures in Children, Ages 4.0-5.11 Years. [Masters Thesis]. Miami University; 2010. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=miami1272376560


University of New South Wales

30. Kyaw Kyaw, Ye Naung. Range and endurance modelling of a multi-engine aircraft with one engine inoperative (oei).

Degree: Engineering & Information Technology Canberra, 2014, University of New South Wales

 When one of the engines on a multi-engine aircraft stops working the one engine inoperative (OEI) condition exists. This causes several negative effects to a… (more)

Subjects/Keywords: Aerodynamic; Flight optmization; Range and Endurance; One Engine Inoperative; Multi-variable Modelling; Aerodynamic

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

APA (6th Edition):

Kyaw Kyaw, Y. N. (2014). Range and endurance modelling of a multi-engine aircraft with one engine inoperative (oei). (Masters Thesis). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/53995 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12706/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Kyaw Kyaw, Ye Naung. “Range and endurance modelling of a multi-engine aircraft with one engine inoperative (oei).” 2014. Masters Thesis, University of New South Wales. Accessed April 23, 2019. http://handle.unsw.edu.au/1959.4/53995 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12706/SOURCE02?view=true.

MLA Handbook (7th Edition):

Kyaw Kyaw, Ye Naung. “Range and endurance modelling of a multi-engine aircraft with one engine inoperative (oei).” 2014. Web. 23 Apr 2019.

Vancouver:

Kyaw Kyaw YN. Range and endurance modelling of a multi-engine aircraft with one engine inoperative (oei). [Internet] [Masters thesis]. University of New South Wales; 2014. [cited 2019 Apr 23]. Available from: http://handle.unsw.edu.au/1959.4/53995 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12706/SOURCE02?view=true.

Council of Science Editors:

Kyaw Kyaw YN. Range and endurance modelling of a multi-engine aircraft with one engine inoperative (oei). [Masters Thesis]. University of New South Wales; 2014. Available from: http://handle.unsw.edu.au/1959.4/53995 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12706/SOURCE02?view=true

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