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You searched for subject:( wing camber ). Showing records 1 – 30 of 820 total matches.

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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

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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 August 19, 2019. 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. 19 Aug 2019.

Vancouver:

Balasubramanian K. Novel, Unified, Curvature-Based Airfoil Parameterization Model for Turbomachinery Blades and Wings. [Internet] [Masters thesis]. University of Cincinnati; 2018. [cited 2019 Aug 19]. 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


University of Dayton

2. Zientarski, Lauren Ann. Wind Tunnel Testing of a Variable Camber Compliant Wing with a Unique Dual Load Cell Test Fixture.

Degree: MS(M.S.), Aerospace Engineering, 2015, University of Dayton

 This thesis describes the design, setup, and testing of a unique mounting fixture built for the Variable Camber Compliant Wing developed by the U.S. Air… (more)

Subjects/Keywords: Aerospace Engineering; Engineering; Variable Camber Compliant Wing; Dual Load Cell; Test Fixture Validation; Calibration Loading

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APA (6th Edition):

Zientarski, L. A. (2015). Wind Tunnel Testing of a Variable Camber Compliant Wing with a Unique Dual Load Cell Test Fixture. (Masters Thesis). University of Dayton. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=dayton1448893315

Chicago Manual of Style (16th Edition):

Zientarski, Lauren Ann. “Wind Tunnel Testing of a Variable Camber Compliant Wing with a Unique Dual Load Cell Test Fixture.” 2015. Masters Thesis, University of Dayton. Accessed August 19, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1448893315.

MLA Handbook (7th Edition):

Zientarski, Lauren Ann. “Wind Tunnel Testing of a Variable Camber Compliant Wing with a Unique Dual Load Cell Test Fixture.” 2015. Web. 19 Aug 2019.

Vancouver:

Zientarski LA. Wind Tunnel Testing of a Variable Camber Compliant Wing with a Unique Dual Load Cell Test Fixture. [Internet] [Masters thesis]. University of Dayton; 2015. [cited 2019 Aug 19]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1448893315.

Council of Science Editors:

Zientarski LA. Wind Tunnel Testing of a Variable Camber Compliant Wing with a Unique Dual Load Cell Test Fixture. [Masters Thesis]. University of Dayton; 2015. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1448893315


University of Kentucky

3. Mahmood, Osamah Ibrahim. CAMBER CONTROL IN SIMPLY SUPPORTED PRESTRESSED CONCRETE BRIDGE GIRDERS.

Degree: 2013, University of Kentucky

 When designing a bridge, serviceability usually controls and is a more important factor than the ultimate capacity of the bridge or the allowable stresses. Therefore,… (more)

Subjects/Keywords: Camber; Camber Control; Civil Engineering

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APA (6th Edition):

Mahmood, O. I. (2013). CAMBER CONTROL IN SIMPLY SUPPORTED PRESTRESSED CONCRETE BRIDGE GIRDERS. (Masters Thesis). University of Kentucky. Retrieved from http://uknowledge.uky.edu/ce_etds/7

Chicago Manual of Style (16th Edition):

Mahmood, Osamah Ibrahim. “CAMBER CONTROL IN SIMPLY SUPPORTED PRESTRESSED CONCRETE BRIDGE GIRDERS.” 2013. Masters Thesis, University of Kentucky. Accessed August 19, 2019. http://uknowledge.uky.edu/ce_etds/7.

MLA Handbook (7th Edition):

Mahmood, Osamah Ibrahim. “CAMBER CONTROL IN SIMPLY SUPPORTED PRESTRESSED CONCRETE BRIDGE GIRDERS.” 2013. Web. 19 Aug 2019.

Vancouver:

Mahmood OI. CAMBER CONTROL IN SIMPLY SUPPORTED PRESTRESSED CONCRETE BRIDGE GIRDERS. [Internet] [Masters thesis]. University of Kentucky; 2013. [cited 2019 Aug 19]. Available from: http://uknowledge.uky.edu/ce_etds/7.

Council of Science Editors:

Mahmood OI. CAMBER CONTROL IN SIMPLY SUPPORTED PRESTRESSED CONCRETE BRIDGE GIRDERS. [Masters Thesis]. University of Kentucky; 2013. Available from: http://uknowledge.uky.edu/ce_etds/7


University of Florida

4. 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

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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 August 19, 2019. 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. 19 Aug 2019.

Vancouver:

Evers BS. Improving Operational Efficiency of Small Unmanned Aircraft Systems for Remote Sensing Applications. [Internet] [Masters thesis]. University of Florida; 2011. [cited 2019 Aug 19]. 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

5. 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

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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 August 19, 2019. 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. 19 Aug 2019.

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 2019 Aug 19]. 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

6. Mistry, Mihir. Quasi-static rotor morphing concepts for rotorcraft performance improvements.

Degree: PhD, Aerospace Engineering, 2012, Penn State University

 The current research is focused on two separate quasi-static rotor morphing concepts: Variable span and variable camber. Both concepts were analyzed from the perspective of… (more)

Subjects/Keywords: rotorcraft; rotor; morphing; smart structure; blade; span; camber; RPM; rotor speed; variation; rotating wing; warping; twist

…6.1.2 System design analysis 6.1.3 Future work . . . . . . 6.2 Variable camber system… …Appendix C Variable camber concept supplementary materials C.1 Airfoil drag polars… …1.40 Timeline of emerging rotor morphing technologies: Var. Chord, Var. Camber and Var. Nose… …1.42 EADS/Eurocopter variable camber system . . . . . . . . . . . . . . 2.1 Schematic… …twist and camber concepts . . . . . . . 127 Proposed variable camber system layout… 

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APA (6th Edition):

Mistry, M. (2012). Quasi-static rotor morphing concepts for rotorcraft performance improvements. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/16272

Chicago Manual of Style (16th Edition):

Mistry, Mihir. “Quasi-static rotor morphing concepts for rotorcraft performance improvements.” 2012. Doctoral Dissertation, Penn State University. Accessed August 19, 2019. https://etda.libraries.psu.edu/catalog/16272.

MLA Handbook (7th Edition):

Mistry, Mihir. “Quasi-static rotor morphing concepts for rotorcraft performance improvements.” 2012. Web. 19 Aug 2019.

Vancouver:

Mistry M. Quasi-static rotor morphing concepts for rotorcraft performance improvements. [Internet] [Doctoral dissertation]. Penn State University; 2012. [cited 2019 Aug 19]. Available from: https://etda.libraries.psu.edu/catalog/16272.

Council of Science Editors:

Mistry M. Quasi-static rotor morphing concepts for rotorcraft performance improvements. [Doctoral Dissertation]. Penn State University; 2012. Available from: https://etda.libraries.psu.edu/catalog/16272


University of Florida

7. 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

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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 August 19, 2019. 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. 19 Aug 2019.

Vancouver:

Lian, Yongsheng ( Author P). Membrane and adaptively-shaped wings for micro air vehicles. [Internet] [Thesis]. University of Florida; 2003. [cited 2019 Aug 19]. 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


Brno University of Technology

8. Marek, Dominik. Vysokovztlaková mechanizace křídel dopravních letadel .

Degree: 2012, Brno University of Technology

 Bakalářská práce utváří přehled používané vysokovztlakové mechanizace na náběžných a odtokových hranách křídel dopravních letadel. Stručně vysvětluje jejich princip činnosti, popisuje výhody a nevýhody jednotlivých… (more)

Subjects/Keywords: Vysokovztlaková mechanizace; klapka; slot; náběžná hrana; odtoková hrana; součinitel vztlaku; úhel náběhu; odpor; pádová rychlost; zakřivení profilu.; High-lift device; flap; slat; leading edge; trailing edge; lift coefficient; angle of attack; drag; stall speed; wing camber.

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APA (6th Edition):

Marek, D. (2012). Vysokovztlaková mechanizace křídel dopravních letadel . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/6116

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):

Marek, Dominik. “Vysokovztlaková mechanizace křídel dopravních letadel .” 2012. Thesis, Brno University of Technology. Accessed August 19, 2019. http://hdl.handle.net/11012/6116.

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

MLA Handbook (7th Edition):

Marek, Dominik. “Vysokovztlaková mechanizace křídel dopravních letadel .” 2012. Web. 19 Aug 2019.

Vancouver:

Marek D. Vysokovztlaková mechanizace křídel dopravních letadel . [Internet] [Thesis]. Brno University of Technology; 2012. [cited 2019 Aug 19]. Available from: http://hdl.handle.net/11012/6116.

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

Council of Science Editors:

Marek D. Vysokovztlaková mechanizace křídel dopravních letadel . [Thesis]. Brno University of Technology; 2012. Available from: http://hdl.handle.net/11012/6116

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


University of Florida

9. Abudaram, Yaakov. Wind Tunnel Testing of Load-Alleviating Membrane Wings.

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

 This work is concerned with wind tunnel testing of elastic latex and silicone membrane wings intended for micro air vehicles. Erratic flow conditions are a… (more)

Subjects/Keywords: Aircraft wings; Bending; Carbon fibers; Geometric angles; Images; Rigid wings; Silicones; Stall; Trailing edges; Wind tunnels; aerodynamic, aeroelastic, alleviating, anisotropic, attack, batten, camber, carbon, chord, deformation, drag, elongation, epoxy, fiber, hyperelastic, latex, leading, lift, mav, membrane, mold, pitching, reynolds, scallop, silicone, stall, sting, trailing, tunnel, vic, vortex, wind, wing

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APA (6th Edition):

Abudaram, Y. (2009). Wind Tunnel Testing of Load-Alleviating Membrane Wings. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0041340

Chicago Manual of Style (16th Edition):

Abudaram, Yaakov. “Wind Tunnel Testing of Load-Alleviating Membrane Wings.” 2009. Masters Thesis, University of Florida. Accessed August 19, 2019. http://ufdc.ufl.edu/UFE0041340.

MLA Handbook (7th Edition):

Abudaram, Yaakov. “Wind Tunnel Testing of Load-Alleviating Membrane Wings.” 2009. Web. 19 Aug 2019.

Vancouver:

Abudaram Y. Wind Tunnel Testing of Load-Alleviating Membrane Wings. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2019 Aug 19]. Available from: http://ufdc.ufl.edu/UFE0041340.

Council of Science Editors:

Abudaram Y. Wind Tunnel Testing of Load-Alleviating Membrane Wings. [Masters Thesis]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0041340


Texas A&M University

10. Cooper, Jacob. Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics.

Degree: 2014, Texas A&M University

 This dissertation investigates high angle of attack delta wing flow at multiple resolutions of turbulence closure. The work is divided into four studies. The objectives… (more)

Subjects/Keywords: delta wing; diamond wing; turbulence model; PANS

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APA (6th Edition):

Cooper, J. (2014). Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/153426

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):

Cooper, Jacob. “Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics.” 2014. Thesis, Texas A&M University. Accessed August 19, 2019. http://hdl.handle.net/1969.1/153426.

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

MLA Handbook (7th Edition):

Cooper, Jacob. “Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics.” 2014. Web. 19 Aug 2019.

Vancouver:

Cooper J. Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics. [Internet] [Thesis]. Texas A&M University; 2014. [cited 2019 Aug 19]. Available from: http://hdl.handle.net/1969.1/153426.

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

Council of Science Editors:

Cooper J. Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics. [Thesis]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/153426

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


University of Manchester

11. Abdul Hamid, Mohd Faisal Bin. Aerodynamic models for insect flight.

Degree: 2016, University of Manchester

 Numerical models of insect flapping flight have previously been developed and used to simulate the performance of insect flight. These models were commonly developed via… (more)

Subjects/Keywords: flapping wing; insect flight; tandem wing

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APA (6th Edition):

Abdul Hamid, M. F. B. (2016). Aerodynamic models for insect flight. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:303191

Chicago Manual of Style (16th Edition):

Abdul Hamid, Mohd Faisal Bin. “Aerodynamic models for insect flight.” 2016. Doctoral Dissertation, University of Manchester. Accessed August 19, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:303191.

MLA Handbook (7th Edition):

Abdul Hamid, Mohd Faisal Bin. “Aerodynamic models for insect flight.” 2016. Web. 19 Aug 2019.

Vancouver:

Abdul Hamid MFB. Aerodynamic models for insect flight. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2019 Aug 19]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:303191.

Council of Science Editors:

Abdul Hamid MFB. Aerodynamic models for insect flight. [Doctoral Dissertation]. University of Manchester; 2016. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:303191


NSYSU

12. Pan, Chih-Hong. A Preliminary Study of Left Wing in Taiwan - from the Perspective of Historical Institutionalism.

Degree: Master, Political Science, 2018, NSYSU

 With the theme of " why did Taiwan not yet have a strong left-wing party?", this paper analyzes the factors behind it and also analyzes… (more)

Subjects/Keywords: class consciousness; left-wing; left-wing party

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APA (6th Edition):

Pan, C. (2018). A Preliminary Study of Left Wing in Taiwan - from the Perspective of Historical Institutionalism. (Thesis). NSYSU. Retrieved from http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0702118-104150

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):

Pan, Chih-Hong. “A Preliminary Study of Left Wing in Taiwan - from the Perspective of Historical Institutionalism.” 2018. Thesis, NSYSU. Accessed August 19, 2019. http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0702118-104150.

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

MLA Handbook (7th Edition):

Pan, Chih-Hong. “A Preliminary Study of Left Wing in Taiwan - from the Perspective of Historical Institutionalism.” 2018. Web. 19 Aug 2019.

Vancouver:

Pan C. A Preliminary Study of Left Wing in Taiwan - from the Perspective of Historical Institutionalism. [Internet] [Thesis]. NSYSU; 2018. [cited 2019 Aug 19]. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0702118-104150.

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

Council of Science Editors:

Pan C. A Preliminary Study of Left Wing in Taiwan - from the Perspective of Historical Institutionalism. [Thesis]. NSYSU; 2018. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0702118-104150

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


University of Manchester

13. Abdul Hamid, Mohd Faisal. Aerodynamic models for insect flight.

Degree: PhD, 2016, University of Manchester

 Numerical models of insect flapping flight have previously been developed and used to simulate the performance of insect flight. These models were commonly developed via… (more)

Subjects/Keywords: 629.13; flapping wing; insect flight; tandem wing

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APA (6th Edition):

Abdul Hamid, M. F. (2016). Aerodynamic models for insect flight. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/aerodynamic-models-for-insect-flight(057be27b-265a-45a0-b8d0-dc3c02a62a77).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728093

Chicago Manual of Style (16th Edition):

Abdul Hamid, Mohd Faisal. “Aerodynamic models for insect flight.” 2016. Doctoral Dissertation, University of Manchester. Accessed August 19, 2019. https://www.research.manchester.ac.uk/portal/en/theses/aerodynamic-models-for-insect-flight(057be27b-265a-45a0-b8d0-dc3c02a62a77).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728093.

MLA Handbook (7th Edition):

Abdul Hamid, Mohd Faisal. “Aerodynamic models for insect flight.” 2016. Web. 19 Aug 2019.

Vancouver:

Abdul Hamid MF. Aerodynamic models for insect flight. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2019 Aug 19]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/aerodynamic-models-for-insect-flight(057be27b-265a-45a0-b8d0-dc3c02a62a77).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728093.

Council of Science Editors:

Abdul Hamid MF. Aerodynamic models for insect flight. [Doctoral Dissertation]. University of Manchester; 2016. Available from: https://www.research.manchester.ac.uk/portal/en/theses/aerodynamic-models-for-insect-flight(057be27b-265a-45a0-b8d0-dc3c02a62a77).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728093


University of Helsinki

14. Pullinen, Leena. Impressions of left-wing and right-wing values, and differences in impressions of left-wing and right-wing values between left-wingers and right-wingers in Finland.

Degree: Institute of Behavioural Sciences; Helsingfors universitet, Beteendevetenskapliga fakulteten, Institutionen för beteendevetenskaper, 2014, University of Helsinki

Aims of the study. The left and right are widely used terms in politics. The terms do not have exact academic definitions, but right-wing stances… (more)

Subjects/Keywords: left-wing; right-wing; values; impressions; Psychology; Psykologia; Psykologi; left-wing; right-wing; values; impressions

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APA (6th Edition):

Pullinen, L. (2014). Impressions of left-wing and right-wing values, and differences in impressions of left-wing and right-wing values between left-wingers and right-wingers in Finland. (Masters Thesis). University of Helsinki. Retrieved from http://hdl.handle.net/10138/154861

Chicago Manual of Style (16th Edition):

Pullinen, Leena. “Impressions of left-wing and right-wing values, and differences in impressions of left-wing and right-wing values between left-wingers and right-wingers in Finland.” 2014. Masters Thesis, University of Helsinki. Accessed August 19, 2019. http://hdl.handle.net/10138/154861.

MLA Handbook (7th Edition):

Pullinen, Leena. “Impressions of left-wing and right-wing values, and differences in impressions of left-wing and right-wing values between left-wingers and right-wingers in Finland.” 2014. Web. 19 Aug 2019.

Vancouver:

Pullinen L. Impressions of left-wing and right-wing values, and differences in impressions of left-wing and right-wing values between left-wingers and right-wingers in Finland. [Internet] [Masters thesis]. University of Helsinki; 2014. [cited 2019 Aug 19]. Available from: http://hdl.handle.net/10138/154861.

Council of Science Editors:

Pullinen L. Impressions of left-wing and right-wing values, and differences in impressions of left-wing and right-wing values between left-wingers and right-wingers in Finland. [Masters Thesis]. University of Helsinki; 2014. Available from: http://hdl.handle.net/10138/154861


University of Kansas

15. Brown, Matthew Alan. A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow.

Degree: MS, Aerospace Engineering, 2013, University of Kansas

 The methods presented in this work are intended to provided an easy to understand and easy to apply method for determining the distributed aerodynamic loads… (more)

Subjects/Keywords: Aerospace engineering; Aerodyanmic loads; Cranked wing; Wing aerodyanmics; Wing loads

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APA (6th Edition):

Brown, M. A. (2013). A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/14195

Chicago Manual of Style (16th Edition):

Brown, Matthew Alan. “A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow.” 2013. Masters Thesis, University of Kansas. Accessed August 19, 2019. http://hdl.handle.net/1808/14195.

MLA Handbook (7th Edition):

Brown, Matthew Alan. “A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow.” 2013. Web. 19 Aug 2019.

Vancouver:

Brown MA. A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow. [Internet] [Masters thesis]. University of Kansas; 2013. [cited 2019 Aug 19]. Available from: http://hdl.handle.net/1808/14195.

Council of Science Editors:

Brown MA. A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow. [Masters Thesis]. University of Kansas; 2013. Available from: http://hdl.handle.net/1808/14195


Linköping University

16. Sohaib, Muhammad. Parameterized Automated Generic Model for Aircraft Wing Structural Design and Mesh Generation for Finite Element Analysis.

Degree: Machine Design, 2011, Linköping University

  This master thesis work presents the development of a parameterized automated generic model for the structural design of an aircraft wing. Furthermore, in order… (more)

Subjects/Keywords: aircraft design; aircraft wing; wing spars; wing ribs; FEM; structural mesh; generic wing model; parametric wing model; automation; design; TECHNOLOGY; TEKNIKVETENSKAP

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APA (6th Edition):

Sohaib, M. (2011). Parameterized Automated Generic Model for Aircraft Wing Structural Design and Mesh Generation for Finite Element Analysis. (Thesis). Linköping University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-71264

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):

Sohaib, Muhammad. “Parameterized Automated Generic Model for Aircraft Wing Structural Design and Mesh Generation for Finite Element Analysis.” 2011. Thesis, Linköping University. Accessed August 19, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-71264.

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

MLA Handbook (7th Edition):

Sohaib, Muhammad. “Parameterized Automated Generic Model for Aircraft Wing Structural Design and Mesh Generation for Finite Element Analysis.” 2011. Web. 19 Aug 2019.

Vancouver:

Sohaib M. Parameterized Automated Generic Model for Aircraft Wing Structural Design and Mesh Generation for Finite Element Analysis. [Internet] [Thesis]. Linköping University; 2011. [cited 2019 Aug 19]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-71264.

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

Council of Science Editors:

Sohaib M. Parameterized Automated Generic Model for Aircraft Wing Structural Design and Mesh Generation for Finite Element Analysis. [Thesis]. Linköping University; 2011. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-71264

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


University of Florida

17. 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

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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 August 19, 2019. 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. 19 Aug 2019.

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 2019 Aug 19]. 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


Texas A&M University

18. Walther, Carolyn Marie. Fundamental Understanding of the Unsteady Aerodynamics of Cycloidal Rotors in Hover at Ultra-Low Reynolds Numbers.

Degree: MS, Aerospace Engineering, 2017, Texas A&M University

 This thesis provides a fundamental understanding of the unsteady aerodynamic phenomena on a cycloidal rotor blade operating at ultra-low Reynolds numbers (Re~18,000) by utilizing a… (more)

Subjects/Keywords: aerodynamics; cycloidal rotors; cyclorotors; PIV; unsteady aerodynamics; virtual camber; vortices; cyclocopters

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APA (6th Edition):

Walther, C. M. (2017). Fundamental Understanding of the Unsteady Aerodynamics of Cycloidal Rotors in Hover at Ultra-Low Reynolds Numbers. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/165824

Chicago Manual of Style (16th Edition):

Walther, Carolyn Marie. “Fundamental Understanding of the Unsteady Aerodynamics of Cycloidal Rotors in Hover at Ultra-Low Reynolds Numbers.” 2017. Masters Thesis, Texas A&M University. Accessed August 19, 2019. http://hdl.handle.net/1969.1/165824.

MLA Handbook (7th Edition):

Walther, Carolyn Marie. “Fundamental Understanding of the Unsteady Aerodynamics of Cycloidal Rotors in Hover at Ultra-Low Reynolds Numbers.” 2017. Web. 19 Aug 2019.

Vancouver:

Walther CM. Fundamental Understanding of the Unsteady Aerodynamics of Cycloidal Rotors in Hover at Ultra-Low Reynolds Numbers. [Internet] [Masters thesis]. Texas A&M University; 2017. [cited 2019 Aug 19]. Available from: http://hdl.handle.net/1969.1/165824.

Council of Science Editors:

Walther CM. Fundamental Understanding of the Unsteady Aerodynamics of Cycloidal Rotors in Hover at Ultra-Low Reynolds Numbers. [Masters Thesis]. Texas A&M University; 2017. Available from: http://hdl.handle.net/1969.1/165824


Virginia Tech

19. 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

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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 August 19, 2019. http://hdl.handle.net/10919/28665.

MLA Handbook (7th Edition):

Bilgen, Onur. “Aerodynamic and Electromechanical Design, Modeling and Implementation Of Piezocomposite Airfoils.” 2010. Web. 19 Aug 2019.

Vancouver:

Bilgen O. Aerodynamic and Electromechanical Design, Modeling and Implementation Of Piezocomposite Airfoils. [Internet] [Doctoral dissertation]. Virginia Tech; 2010. [cited 2019 Aug 19]. 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


Virginia Tech

20. Bert, Stephen M. Using Maturity to Predict Girder Camber.

Degree: MS, Civil Engineering, 2005, Virginia Tech

 The objective of this research was to determine if differential camber of prestressed concrete girders could be reduced by accurate prediction of initial camber at… (more)

Subjects/Keywords: Modulus of Elasticity; Maturity; Camber

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APA (6th Edition):

Bert, S. M. (2005). Using Maturity to Predict Girder Camber. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/32852

Chicago Manual of Style (16th Edition):

Bert, Stephen M. “Using Maturity to Predict Girder Camber.” 2005. Masters Thesis, Virginia Tech. Accessed August 19, 2019. http://hdl.handle.net/10919/32852.

MLA Handbook (7th Edition):

Bert, Stephen M. “Using Maturity to Predict Girder Camber.” 2005. Web. 19 Aug 2019.

Vancouver:

Bert SM. Using Maturity to Predict Girder Camber. [Internet] [Masters thesis]. Virginia Tech; 2005. [cited 2019 Aug 19]. Available from: http://hdl.handle.net/10919/32852.

Council of Science Editors:

Bert SM. Using Maturity to Predict Girder Camber. [Masters Thesis]. Virginia Tech; 2005. Available from: http://hdl.handle.net/10919/32852


Delft University of Technology

21. Roethof, D.N. Influence of active camber control on steering feel:.

Degree: 2016, Delft University of Technology

 Active camber control is a novel suspension control method which can improve the lateral forces on the tires of a vehicle. The mechanism actively tilts… (more)

Subjects/Keywords: active camber; automotive; tire tilt; human in the loop

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APA (6th Edition):

Roethof, D. N. (2016). Influence of active camber control on steering feel:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:0db08bf4-f6aa-46a4-9c3a-2f1aca12f448

Chicago Manual of Style (16th Edition):

Roethof, D N. “Influence of active camber control on steering feel:.” 2016. Masters Thesis, Delft University of Technology. Accessed August 19, 2019. http://resolver.tudelft.nl/uuid:0db08bf4-f6aa-46a4-9c3a-2f1aca12f448.

MLA Handbook (7th Edition):

Roethof, D N. “Influence of active camber control on steering feel:.” 2016. Web. 19 Aug 2019.

Vancouver:

Roethof DN. Influence of active camber control on steering feel:. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2019 Aug 19]. Available from: http://resolver.tudelft.nl/uuid:0db08bf4-f6aa-46a4-9c3a-2f1aca12f448.

Council of Science Editors:

Roethof DN. Influence of active camber control on steering feel:. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:0db08bf4-f6aa-46a4-9c3a-2f1aca12f448


Utah State University

22. Pickett, Ethan. The Short and Long-Term Effects of Temperature and Strain on a Concrete Bulb-Tree Girder Bridge.

Degree: MS, Civil and Environmental Engineering, 2017, Utah State University

  The Utah Transportation Center (UTC) as well as the Mountain Plains Consortium, sponsored a study to investigate the long-term performance of a deck bulb… (more)

Subjects/Keywords: Strain; Gradient; Camber; Prestress; Rain Flow; Civil and Environmental Engineering; Engineering

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APA (6th Edition):

Pickett, E. (2017). The Short and Long-Term Effects of Temperature and Strain on a Concrete Bulb-Tree Girder Bridge. (Masters Thesis). Utah State University. Retrieved from https://digitalcommons.usu.edu/etd/5811

Chicago Manual of Style (16th Edition):

Pickett, Ethan. “The Short and Long-Term Effects of Temperature and Strain on a Concrete Bulb-Tree Girder Bridge.” 2017. Masters Thesis, Utah State University. Accessed August 19, 2019. https://digitalcommons.usu.edu/etd/5811.

MLA Handbook (7th Edition):

Pickett, Ethan. “The Short and Long-Term Effects of Temperature and Strain on a Concrete Bulb-Tree Girder Bridge.” 2017. Web. 19 Aug 2019.

Vancouver:

Pickett E. The Short and Long-Term Effects of Temperature and Strain on a Concrete Bulb-Tree Girder Bridge. [Internet] [Masters thesis]. Utah State University; 2017. [cited 2019 Aug 19]. Available from: https://digitalcommons.usu.edu/etd/5811.

Council of Science Editors:

Pickett E. The Short and Long-Term Effects of Temperature and Strain on a Concrete Bulb-Tree Girder Bridge. [Masters Thesis]. Utah State University; 2017. Available from: https://digitalcommons.usu.edu/etd/5811


University of Minnesota

23. Swenson, Tanner. Effect of Temperature on Prestressed Concrete Bridge Girder Strand Stress during Fabrication.

Degree: MS, Civil Engineering, 2015, University of Minnesota

 The Minnesota Department of Transportation has reported erection cambers of many prestressed concrete bridge girders that were much lower than anticipated. A previous University of… (more)

Subjects/Keywords: camber; experiment; fabrication; prestressed bridge girders; prestress losses; temperature

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APA (6th Edition):

Swenson, T. (2015). Effect of Temperature on Prestressed Concrete Bridge Girder Strand Stress during Fabrication. (Masters Thesis). University of Minnesota. Retrieved from http://hdl.handle.net/11299/175720

Chicago Manual of Style (16th Edition):

Swenson, Tanner. “Effect of Temperature on Prestressed Concrete Bridge Girder Strand Stress during Fabrication.” 2015. Masters Thesis, University of Minnesota. Accessed August 19, 2019. http://hdl.handle.net/11299/175720.

MLA Handbook (7th Edition):

Swenson, Tanner. “Effect of Temperature on Prestressed Concrete Bridge Girder Strand Stress during Fabrication.” 2015. Web. 19 Aug 2019.

Vancouver:

Swenson T. Effect of Temperature on Prestressed Concrete Bridge Girder Strand Stress during Fabrication. [Internet] [Masters thesis]. University of Minnesota; 2015. [cited 2019 Aug 19]. Available from: http://hdl.handle.net/11299/175720.

Council of Science Editors:

Swenson T. Effect of Temperature on Prestressed Concrete Bridge Girder Strand Stress during Fabrication. [Masters Thesis]. University of Minnesota; 2015. Available from: http://hdl.handle.net/11299/175720


Indian Institute of Science

24. Mukherjee, Sujoy. Structural Modeling And Analysis Of Insect Scale Flapping Wing.

Degree: 2012, Indian Institute of Science

 Micro Air Vehicles (MAVs) are defined as a class of vehicles with their larger dimension not exceeding 15 cm and weighing 100 gm. The three… (more)

Subjects/Keywords: Flapping Wing; Micro Air Vehicles (MAVs); Calliphora Wing; Flapping Wings; Twisting Wing; Flapping Flight; Aeronautics

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APA (6th Edition):

Mukherjee, S. (2012). Structural Modeling And Analysis Of Insect Scale Flapping Wing. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2021

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):

Mukherjee, Sujoy. “Structural Modeling And Analysis Of Insect Scale Flapping Wing.” 2012. Thesis, Indian Institute of Science. Accessed August 19, 2019. http://hdl.handle.net/2005/2021.

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

MLA Handbook (7th Edition):

Mukherjee, Sujoy. “Structural Modeling And Analysis Of Insect Scale Flapping Wing.” 2012. Web. 19 Aug 2019.

Vancouver:

Mukherjee S. Structural Modeling And Analysis Of Insect Scale Flapping Wing. [Internet] [Thesis]. Indian Institute of Science; 2012. [cited 2019 Aug 19]. Available from: http://hdl.handle.net/2005/2021.

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

Council of Science Editors:

Mukherjee S. Structural Modeling And Analysis Of Insect Scale Flapping Wing. [Thesis]. Indian Institute of Science; 2012. Available from: http://hdl.handle.net/2005/2021

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


Indian Institute of Science

25. Mukherjee, Sujoy. Structural Modeling And Analysis Of Insect Scale Flapping Wing.

Degree: 2012, Indian Institute of Science

 Micro Air Vehicles (MAVs) are defined as a class of vehicles with their larger dimension not exceeding 15 cm and weighing 100 gm. The three… (more)

Subjects/Keywords: Flapping Wing; Micro Air Vehicles (MAVs); Calliphora Wing; Flapping Wings; Twisting Wing; Flapping Flight; Aeronautics

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APA (6th Edition):

Mukherjee, S. (2012). Structural Modeling And Analysis Of Insect Scale Flapping Wing. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/2021 ; http://etd.ncsi.iisc.ernet.in/abstracts/2616/G24985-Abs.pdf

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):

Mukherjee, Sujoy. “Structural Modeling And Analysis Of Insect Scale Flapping Wing.” 2012. Thesis, Indian Institute of Science. Accessed August 19, 2019. http://etd.iisc.ernet.in/handle/2005/2021 ; http://etd.ncsi.iisc.ernet.in/abstracts/2616/G24985-Abs.pdf.

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

MLA Handbook (7th Edition):

Mukherjee, Sujoy. “Structural Modeling And Analysis Of Insect Scale Flapping Wing.” 2012. Web. 19 Aug 2019.

Vancouver:

Mukherjee S. Structural Modeling And Analysis Of Insect Scale Flapping Wing. [Internet] [Thesis]. Indian Institute of Science; 2012. [cited 2019 Aug 19]. Available from: http://etd.iisc.ernet.in/handle/2005/2021 ; http://etd.ncsi.iisc.ernet.in/abstracts/2616/G24985-Abs.pdf.

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

Council of Science Editors:

Mukherjee S. Structural Modeling And Analysis Of Insect Scale Flapping Wing. [Thesis]. Indian Institute of Science; 2012. Available from: http://etd.iisc.ernet.in/handle/2005/2021 ; http://etd.ncsi.iisc.ernet.in/abstracts/2616/G24985-Abs.pdf

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


Carnegie Mellon University

26. Colmenares, David. Design and Control of a Resonant, Flapping Wing Micro Aerial Vehicle Capable of Controlled Flight.

Degree: 2017, Carnegie Mellon University

 Small scale unmanned aircraft, such as quadrotors, that are quickly emerging as versatile tools for a wide range of applications including search and rescue, hazardous… (more)

Subjects/Keywords: Micro Aerial Vehicle; Flapping wing; Resonant Actuator; DC motor; Thermal Model; Flexible Wing; Wing Twist

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APA (6th Edition):

Colmenares, D. (2017). Design and Control of a Resonant, Flapping Wing Micro Aerial Vehicle Capable of Controlled Flight. (Thesis). Carnegie Mellon University. Retrieved from http://repository.cmu.edu/dissertations/1032

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):

Colmenares, David. “Design and Control of a Resonant, Flapping Wing Micro Aerial Vehicle Capable of Controlled Flight.” 2017. Thesis, Carnegie Mellon University. Accessed August 19, 2019. http://repository.cmu.edu/dissertations/1032.

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

MLA Handbook (7th Edition):

Colmenares, David. “Design and Control of a Resonant, Flapping Wing Micro Aerial Vehicle Capable of Controlled Flight.” 2017. Web. 19 Aug 2019.

Vancouver:

Colmenares D. Design and Control of a Resonant, Flapping Wing Micro Aerial Vehicle Capable of Controlled Flight. [Internet] [Thesis]. Carnegie Mellon University; 2017. [cited 2019 Aug 19]. Available from: http://repository.cmu.edu/dissertations/1032.

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

Council of Science Editors:

Colmenares D. Design and Control of a Resonant, Flapping Wing Micro Aerial Vehicle Capable of Controlled Flight. [Thesis]. Carnegie Mellon University; 2017. Available from: http://repository.cmu.edu/dissertations/1032

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


University of Manchester

27. El Ouardi, Othman. Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism.

Degree: 2014, University of Manchester

Wing morphing has the potential to significantly improve the performance of an aircraft. The aerospace industry currently relies on control surfaces for changing aircraft wing(more)

Subjects/Keywords: Morphing wing; Adaptive wing; SMA; Variable thickness wing; Shape morphing; Smart materials

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APA (6th Edition):

El Ouardi, O. (2014). Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:237682

Chicago Manual of Style (16th Edition):

El Ouardi, Othman. “Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism.” 2014. Doctoral Dissertation, University of Manchester. Accessed August 19, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:237682.

MLA Handbook (7th Edition):

El Ouardi, Othman. “Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism.” 2014. Web. 19 Aug 2019.

Vancouver:

El Ouardi O. Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism. [Internet] [Doctoral dissertation]. University of Manchester; 2014. [cited 2019 Aug 19]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:237682.

Council of Science Editors:

El Ouardi O. Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism. [Doctoral Dissertation]. University of Manchester; 2014. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:237682


Texas A&M University

28. Jackson, Justin Patrick. Modelling and control of a symmetric flapping wing vehicle: an optimal control approach.

Degree: 2009, Texas A&M University

 This thesis presents a method for designing a flapping wing stroke for a flapping wing vehicle. A flapping wing vehicle is a vehicle such as… (more)

Subjects/Keywords: flapping wing; control; optimal

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APA (6th Edition):

Jackson, J. P. (2009). Modelling and control of a symmetric flapping wing vehicle: an optimal control approach. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2854

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):

Jackson, Justin Patrick. “Modelling and control of a symmetric flapping wing vehicle: an optimal control approach.” 2009. Thesis, Texas A&M University. Accessed August 19, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2854.

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

MLA Handbook (7th Edition):

Jackson, Justin Patrick. “Modelling and control of a symmetric flapping wing vehicle: an optimal control approach.” 2009. Web. 19 Aug 2019.

Vancouver:

Jackson JP. Modelling and control of a symmetric flapping wing vehicle: an optimal control approach. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2019 Aug 19]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2854.

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

Council of Science Editors:

Jackson JP. Modelling and control of a symmetric flapping wing vehicle: an optimal control approach. [Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2854

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


Virginia Tech

29. Eger, Charles Alfred Gaitan. Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects.

Degree: MS, Aerospace and Ocean Engineering, 2013, Virginia Tech

 A procedure for the design of a scaled aircraft using linear aeroelastic scaling is developed and demonstrated. Previous work has shown the viability in matching… (more)

Subjects/Keywords: Aeroelasticity; Scaling; Joined-wing

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

APA (6th Edition):

Eger, C. A. G. (2013). Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/23088

Chicago Manual of Style (16th Edition):

Eger, Charles Alfred Gaitan. “Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects.” 2013. Masters Thesis, Virginia Tech. Accessed August 19, 2019. http://hdl.handle.net/10919/23088.

MLA Handbook (7th Edition):

Eger, Charles Alfred Gaitan. “Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects.” 2013. Web. 19 Aug 2019.

Vancouver:

Eger CAG. Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2019 Aug 19]. Available from: http://hdl.handle.net/10919/23088.

Council of Science Editors:

Eger CAG. Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects. [Masters Thesis]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/23088


Delft University of Technology

30. Riahi, G. Model Order Reduction for a Nonlinear Finite Element Model of a Joined Wing Structure:.

Degree: 2012, Delft University of Technology

 Joined Wing is a concept of nonplanar airplane wing structure. This is a new concept which is not yet used for commercial airplanes but has… (more)

Subjects/Keywords: nonlinear; finite; wing structure

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Riahi, G. (2012). Model Order Reduction for a Nonlinear Finite Element Model of a Joined Wing Structure:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:ab0d4288-3dfd-468d-a6d8-cdafa3ea2164

Chicago Manual of Style (16th Edition):

Riahi, G. “Model Order Reduction for a Nonlinear Finite Element Model of a Joined Wing Structure:.” 2012. Masters Thesis, Delft University of Technology. Accessed August 19, 2019. http://resolver.tudelft.nl/uuid:ab0d4288-3dfd-468d-a6d8-cdafa3ea2164.

MLA Handbook (7th Edition):

Riahi, G. “Model Order Reduction for a Nonlinear Finite Element Model of a Joined Wing Structure:.” 2012. Web. 19 Aug 2019.

Vancouver:

Riahi G. Model Order Reduction for a Nonlinear Finite Element Model of a Joined Wing Structure:. [Internet] [Masters thesis]. Delft University of Technology; 2012. [cited 2019 Aug 19]. Available from: http://resolver.tudelft.nl/uuid:ab0d4288-3dfd-468d-a6d8-cdafa3ea2164.

Council of Science Editors:

Riahi G. Model Order Reduction for a Nonlinear Finite Element Model of a Joined Wing Structure:. [Masters Thesis]. Delft University of Technology; 2012. Available from: http://resolver.tudelft.nl/uuid:ab0d4288-3dfd-468d-a6d8-cdafa3ea2164

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