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:(Airfoil camber). Showing records 1 – 10 of 10 total matches.

Search Limiters

Last 2 Years | English Only

No search limiters apply to these results.

▼ Search Limiters


University of Cincinnati

1. Balasubramanian, Karthik. Novel, Unified, Curvature-Based Airfoil Parameterization Model for Turbomachinery Blades and Wings.

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

 The predictable effect of surface curvature on the contiguous streamtube allows for the use of geometric curvature as a direct and aerodynamically meaningful parametric model… (more)

Subjects/Keywords: Aerospace Materials; Optimization; Airfoil; Turbomachinery; Wing; Curvature; Camber line and thickness

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Balasubramanian, K. (2018). Novel, Unified, Curvature-Based Airfoil Parameterization Model for Turbomachinery Blades and Wings. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1535459266289742

Chicago Manual of Style (16th Edition):

Balasubramanian, Karthik. “Novel, Unified, Curvature-Based Airfoil Parameterization Model for Turbomachinery Blades and Wings.” 2018. Masters Thesis, University of Cincinnati. Accessed April 08, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1535459266289742.

MLA Handbook (7th Edition):

Balasubramanian, Karthik. “Novel, Unified, Curvature-Based Airfoil Parameterization Model for Turbomachinery Blades and Wings.” 2018. Web. 08 Apr 2020.

Vancouver:

Balasubramanian K. Novel, Unified, Curvature-Based Airfoil Parameterization Model for Turbomachinery Blades and Wings. [Internet] [Masters thesis]. University of Cincinnati; 2018. [cited 2020 Apr 08]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1535459266289742.

Council of Science Editors:

Balasubramanian K. Novel, Unified, Curvature-Based Airfoil Parameterization Model for Turbomachinery Blades and Wings. [Masters Thesis]. University of Cincinnati; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1535459266289742


Virginia Tech

2. Bilgen, Onur. Aerodynamic and Electromechanical Design, Modeling and Implementation Of Piezocomposite Airfoils.

Degree: PhD, Mechanical Engineering, 2010, Virginia Tech

 Piezoelectrics offer high actuation authority and sensing over a wide range of frequencies. A Macro-Fiber Composite is a type of piezoelectric device that offers structural… (more)

Subjects/Keywords: Bimorph; Unimorph; Macro-Fiber Composite; Variable-Camber Airfoil; Piezoceramic

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Bilgen, O. (2010). Aerodynamic and Electromechanical Design, Modeling and Implementation Of Piezocomposite Airfoils. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/28665

Chicago Manual of Style (16th Edition):

Bilgen, Onur. “Aerodynamic and Electromechanical Design, Modeling and Implementation Of Piezocomposite Airfoils.” 2010. Doctoral Dissertation, Virginia Tech. Accessed April 08, 2020. http://hdl.handle.net/10919/28665.

MLA Handbook (7th Edition):

Bilgen, Onur. “Aerodynamic and Electromechanical Design, Modeling and Implementation Of Piezocomposite Airfoils.” 2010. Web. 08 Apr 2020.

Vancouver:

Bilgen O. Aerodynamic and Electromechanical Design, Modeling and Implementation Of Piezocomposite Airfoils. [Internet] [Doctoral dissertation]. Virginia Tech; 2010. [cited 2020 Apr 08]. Available from: http://hdl.handle.net/10919/28665.

Council of Science Editors:

Bilgen O. Aerodynamic and Electromechanical Design, Modeling and Implementation Of Piezocomposite Airfoils. [Doctoral Dissertation]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/28665

3. Li, Daxin. Multi-objective design optimization for high-lift aircraft configurations supported by surrogate modeling.

Degree: MSc by Research, 2013, Cranfield University

 Nowadays, the competition among airlines seriously depend upon the saving operating costs, with the premise that not to degrade its services quality. Especially in the… (more)

Subjects/Keywords: Airfoil Design; Supercritical Airfoil; Multi-element airfoil parameter; Variable Camber Airfoil; Droppable spoiler; Aerodynamic design

…15 Figure 2-13: Aerodynamic efficiency improves from variable camber airfoil [39]… …19: Variable camber airfoil [44]… …18 Figure 2-20: Variable camber airfoil [39]… …ratio elastic wing; and variable airfoil camber continuous trailing edge flap. 8 2.3.1.1… …downward deflection to achieve airfoil variable camber function [38], so the whole fly… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Li, D. (2013). Multi-objective design optimization for high-lift aircraft configurations supported by surrogate modeling. (Masters Thesis). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/8468

Chicago Manual of Style (16th Edition):

Li, Daxin. “Multi-objective design optimization for high-lift aircraft configurations supported by surrogate modeling.” 2013. Masters Thesis, Cranfield University. Accessed April 08, 2020. http://dspace.lib.cranfield.ac.uk/handle/1826/8468.

MLA Handbook (7th Edition):

Li, Daxin. “Multi-objective design optimization for high-lift aircraft configurations supported by surrogate modeling.” 2013. Web. 08 Apr 2020.

Vancouver:

Li D. Multi-objective design optimization for high-lift aircraft configurations supported by surrogate modeling. [Internet] [Masters thesis]. Cranfield University; 2013. [cited 2020 Apr 08]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/8468.

Council of Science Editors:

Li D. Multi-objective design optimization for high-lift aircraft configurations supported by surrogate modeling. [Masters Thesis]. Cranfield University; 2013. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/8468


University of Florida

4. Patil, Abhishek. Buckling Analysis of a Bendable Composite Unmanned Air Vehicle Wing.

Degree: MS, Mechanical Engineering - Mechanical and Aerospace Engineering, 2009, University of Florida

 The bendable UAV wing developed by researchers at the University of Florida has the ability to load stiffen in the positive load direction and at… (more)

Subjects/Keywords: Aircraft wings; Airfoil camber; Airfoils; Buckling; Eigenvalues; Load carrying capacity; Modeling; Remotely piloted vehicles; Structural deflection; Velocity; abhishek, analysis, bendable, buckling, expermiental, ifju, mav, patil, predictor, stress, tool, uav, ufl

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Patil, A. (2009). Buckling Analysis of a Bendable Composite Unmanned Air Vehicle Wing. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0025037

Chicago Manual of Style (16th Edition):

Patil, Abhishek. “Buckling Analysis of a Bendable Composite Unmanned Air Vehicle Wing.” 2009. Masters Thesis, University of Florida. Accessed April 08, 2020. http://ufdc.ufl.edu/UFE0025037.

MLA Handbook (7th Edition):

Patil, Abhishek. “Buckling Analysis of a Bendable Composite Unmanned Air Vehicle Wing.” 2009. Web. 08 Apr 2020.

Vancouver:

Patil A. Buckling Analysis of a Bendable Composite Unmanned Air Vehicle Wing. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2020 Apr 08]. Available from: http://ufdc.ufl.edu/UFE0025037.

Council of Science Editors:

Patil A. Buckling Analysis of a Bendable Composite Unmanned Air Vehicle Wing. [Masters Thesis]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0025037


University of Florida

5. Evers, Brandon S. Improving Operational Efficiency of Small Unmanned Aircraft Systems for Remote Sensing Applications.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2011, University of Florida

 Aerial photogrammetry is traditionally a specialized application for small manned aircraft with large operating expenses. Emerging small unmanned aerial systems (sUAS) have the capability to… (more)

Subjects/Keywords: Aircraft wings; Airfoil camber; Airspeed; Cruises; Fuselages; Payloads; Remote sensing; Remotely piloted vehicles; Takeoff; Wing flaps; aerial  – aircraft  – autonomous  – flight  – photogrammetry  – planning  – remote  – sensing  – systems  – uas  – uav  – unmanned

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Evers, B. S. (2011). Improving Operational Efficiency of Small Unmanned Aircraft Systems for Remote Sensing Applications. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0043857

Chicago Manual of Style (16th Edition):

Evers, Brandon S. “Improving Operational Efficiency of Small Unmanned Aircraft Systems for Remote Sensing Applications.” 2011. Masters Thesis, University of Florida. Accessed April 08, 2020. http://ufdc.ufl.edu/UFE0043857.

MLA Handbook (7th Edition):

Evers, Brandon S. “Improving Operational Efficiency of Small Unmanned Aircraft Systems for Remote Sensing Applications.” 2011. Web. 08 Apr 2020.

Vancouver:

Evers BS. Improving Operational Efficiency of Small Unmanned Aircraft Systems for Remote Sensing Applications. [Internet] [Masters thesis]. University of Florida; 2011. [cited 2020 Apr 08]. Available from: http://ufdc.ufl.edu/UFE0043857.

Council of Science Editors:

Evers BS. Improving Operational Efficiency of Small Unmanned Aircraft Systems for Remote Sensing Applications. [Masters Thesis]. University of Florida; 2011. Available from: http://ufdc.ufl.edu/UFE0043857


University of Florida

6. Arce, Manuel A. Passively Compliant Membranes in Low Aspect Ratio Wings.

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

 The study of mammalian flight has led to the design of bio inspired micro air vehicles. These micro air vehicles utilize passively compliant membranes to… (more)

Subjects/Keywords: Aerodynamics; Aircraft wings; Airfoil camber; Flat plates; Flow distribution; Near wakes; P branes; Structural deflection; Trailing edges; Velocity; batten-reinforced  – compliant  – fluid-structure  – mav  – membrane

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Arce, M. A. (2013). Passively Compliant Membranes in Low Aspect Ratio Wings. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0046357

Chicago Manual of Style (16th Edition):

Arce, Manuel A. “Passively Compliant Membranes in Low Aspect Ratio Wings.” 2013. Masters Thesis, University of Florida. Accessed April 08, 2020. http://ufdc.ufl.edu/UFE0046357.

MLA Handbook (7th Edition):

Arce, Manuel A. “Passively Compliant Membranes in Low Aspect Ratio Wings.” 2013. Web. 08 Apr 2020.

Vancouver:

Arce MA. Passively Compliant Membranes in Low Aspect Ratio Wings. [Internet] [Masters thesis]. University of Florida; 2013. [cited 2020 Apr 08]. Available from: http://ufdc.ufl.edu/UFE0046357.

Council of Science Editors:

Arce MA. Passively Compliant Membranes in Low Aspect Ratio Wings. [Masters Thesis]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0046357


University of Florida

7. Jagdale, Vijay. Experimental Characterization and Multidisciplinary Conceptual Design Optimization of a Bendable Load Stiffened Unmanned Air Vehicle Wing.

Degree: PhD, Mechanical Engineering - Mechanical and Aerospace Engineering, 2010, University of Florida

 Demand for deployable MAVs and UAVs with wings designed to reduce aircraft storage volume led to the development of a bendable wing concept at the… (more)

Subjects/Keywords: Aerodynamics; Aircraft wings; Airfoil camber; Airfoils; Buckling; Design optimization; Modeling; Remotely piloted vehicles; Sweepback; Velocity; aircraft, bendable, buckling, compact, compliant, design, experimental, foldable, mav, optimization, storage, uav, unmanned, wing

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Jagdale, V. (2010). Experimental Characterization and Multidisciplinary Conceptual Design Optimization of a Bendable Load Stiffened Unmanned Air Vehicle Wing. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0042430

Chicago Manual of Style (16th Edition):

Jagdale, Vijay. “Experimental Characterization and Multidisciplinary Conceptual Design Optimization of a Bendable Load Stiffened Unmanned Air Vehicle Wing.” 2010. Doctoral Dissertation, University of Florida. Accessed April 08, 2020. http://ufdc.ufl.edu/UFE0042430.

MLA Handbook (7th Edition):

Jagdale, Vijay. “Experimental Characterization and Multidisciplinary Conceptual Design Optimization of a Bendable Load Stiffened Unmanned Air Vehicle Wing.” 2010. Web. 08 Apr 2020.

Vancouver:

Jagdale V. Experimental Characterization and Multidisciplinary Conceptual Design Optimization of a Bendable Load Stiffened Unmanned Air Vehicle Wing. [Internet] [Doctoral dissertation]. University of Florida; 2010. [cited 2020 Apr 08]. Available from: http://ufdc.ufl.edu/UFE0042430.

Council of Science Editors:

Jagdale V. Experimental Characterization and Multidisciplinary Conceptual Design Optimization of a Bendable Load Stiffened Unmanned Air Vehicle Wing. [Doctoral Dissertation]. University of Florida; 2010. Available from: http://ufdc.ufl.edu/UFE0042430


University of Florida

8. Lian, Yongsheng ( Author, Primary ). Membrane and adaptively-shaped wings for micro air vehicles.

Degree: 2003, University of Florida

Subjects/Keywords: Aerodynamics; Aircraft wings; Airfoil camber; Coordinate systems; Low reynolds number; Rigid wings; Shape optimization; Turbulence models; Velocity; Wing flaps

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Lian, Yongsheng ( Author, P. ). (2003). Membrane and adaptively-shaped wings for micro air vehicles. (Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0001085

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):

Lian, Yongsheng ( Author, Primary ). “Membrane and adaptively-shaped wings for micro air vehicles.” 2003. Thesis, University of Florida. Accessed April 08, 2020. http://ufdc.ufl.edu/UFE0001085.

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

MLA Handbook (7th Edition):

Lian, Yongsheng ( Author, Primary ). “Membrane and adaptively-shaped wings for micro air vehicles.” 2003. Web. 08 Apr 2020.

Vancouver:

Lian, Yongsheng ( Author P). Membrane and adaptively-shaped wings for micro air vehicles. [Internet] [Thesis]. University of Florida; 2003. [cited 2020 Apr 08]. Available from: http://ufdc.ufl.edu/UFE0001085.

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

Council of Science Editors:

Lian, Yongsheng ( Author P). Membrane and adaptively-shaped wings for micro air vehicles. [Thesis]. University of Florida; 2003. Available from: http://ufdc.ufl.edu/UFE0001085

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


North Carolina State University

9. McAvoy, Christopher William. Analytical and Experimental Approaches to Airfoil-Aircraft Design Integration.

Degree: MS, Aerospace Engineering, 2002, North Carolina State University

 The aerodynamic characteristics of the wing airfoil are critical to achieving desired aircraft performance. However, even with all of the advances in airfoil and aircraft… (more)

Subjects/Keywords: aircraft performance; airfoil; aircraft; design; newton method; optimization; laminar flow; cruise flap; automatic flap; camber; trailing-edge flap; subsonic; general aviation; thin airfoil theory; UAV; stagnation point; low speed flow; low reynolds number; wind tunnel; NLF; drag polar; drag bucket; XFOIL; low-drag range; design integration; aerospace engineering; aeronautical; airfoil model construction; pressure distributions; trim effects; trim considerations; surface pressure sensing

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

McAvoy, C. W. (2002). Analytical and Experimental Approaches to Airfoil-Aircraft Design Integration. (Thesis). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/7

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):

McAvoy, Christopher William. “Analytical and Experimental Approaches to Airfoil-Aircraft Design Integration.” 2002. Thesis, North Carolina State University. Accessed April 08, 2020. http://www.lib.ncsu.edu/resolver/1840.16/7.

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

MLA Handbook (7th Edition):

McAvoy, Christopher William. “Analytical and Experimental Approaches to Airfoil-Aircraft Design Integration.” 2002. Web. 08 Apr 2020.

Vancouver:

McAvoy CW. Analytical and Experimental Approaches to Airfoil-Aircraft Design Integration. [Internet] [Thesis]. North Carolina State University; 2002. [cited 2020 Apr 08]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/7.

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

Council of Science Editors:

McAvoy CW. Analytical and Experimental Approaches to Airfoil-Aircraft Design Integration. [Thesis]. North Carolina State University; 2002. Available from: http://www.lib.ncsu.edu/resolver/1840.16/7

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


University of Florida

10. Boria, Frank J. Optimization of a Morphing Wing Geometry Using a Genetic Algorithm with Wind Tunnel Hardware-in-the-Loop.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2007, University of Florida

 Advancements of compliant actuator technologies and flexible composite structures have enabled true wing morphing capabilities. The resultant effect of these new capabilities is optimal wing… (more)

Subjects/Keywords: Aerodynamic coefficients; Aerodynamics; Aircraft wings; Airfoil camber; Airfoils; Drag coefficient; Genetic algorithms; Servomotors; Three dimensional imaging; Wind tunnels; aerodynamic, air, aircraft, algorithm, biorobots, boria, change, composite, dic, ga, genetic, hardware, loop, mav, morph, morphing, optimization, shape, uav, vehicle, vic, wing

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Boria, F. J. (2007). Optimization of a Morphing Wing Geometry Using a Genetic Algorithm with Wind Tunnel Hardware-in-the-Loop. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0021478

Chicago Manual of Style (16th Edition):

Boria, Frank J. “Optimization of a Morphing Wing Geometry Using a Genetic Algorithm with Wind Tunnel Hardware-in-the-Loop.” 2007. Masters Thesis, University of Florida. Accessed April 08, 2020. http://ufdc.ufl.edu/UFE0021478.

MLA Handbook (7th Edition):

Boria, Frank J. “Optimization of a Morphing Wing Geometry Using a Genetic Algorithm with Wind Tunnel Hardware-in-the-Loop.” 2007. Web. 08 Apr 2020.

Vancouver:

Boria FJ. Optimization of a Morphing Wing Geometry Using a Genetic Algorithm with Wind Tunnel Hardware-in-the-Loop. [Internet] [Masters thesis]. University of Florida; 2007. [cited 2020 Apr 08]. Available from: http://ufdc.ufl.edu/UFE0021478.

Council of Science Editors:

Boria FJ. Optimization of a Morphing Wing Geometry Using a Genetic Algorithm with Wind Tunnel Hardware-in-the-Loop. [Masters Thesis]. University of Florida; 2007. Available from: http://ufdc.ufl.edu/UFE0021478

.