Design and flight testing of inflatable wings with wing warping

SAE Technical Papers

Volumn , Issue , 2005, Pages

  Jacob, Jamey D ^a   Simpson, Andrew ^a   Smith, Suzanne ^a  

^a UNIVERSITY OF KENTUCKY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; DEFORMATION;

AERODYNAMIC EFFICIENCY; AERODYNAMIC FORCES; DESIGN AND CONSTRUCTION; EXTERNAL LOADS; FLIGHT TESTING; INFLATABLE WINGS; MECHANICAL MANIPULATION; RECENT RESEARCHES;

ANTENNAS;

EID: 85072483556     PISSN: 01487191     EISSN: 26883627     Source Type: Journal    
DOI: 10.4271/2005-01-3392     Document Type: Conference Paper

References (24)

1. Jenkins, C.H., (Ed.), Gossamer Spacecraft: Membrane/Inflatable Structures Technologies for Space Applications, AIAA, Washington, DC, 2001.
2. Cadogan, D., Smith, T., Lee, R., Scarborough, S., Graziosi, D., "Inflatable and Rigidizable Wing Components for Unmanned Aerial Vehicles," AIAA No. AIAA-2003-6630, 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Norfolk, VA, April 2003.
3. Murray, J., Pahle, J., Thornton, S., Frackowiak, T., Mello, J., and Norton, B., "Ground and Flight Evaluation of a Small-Scale Inflatable-Winged Aircraft." AIAA 2002-0820, 40th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, Jan. 14-17, 2005.
4. Lin, J.K., Sapna, G.H., Cadogan, D.P., Scar-borough, S.E., "Inflatable Rigidizable Isogrid Boom Development," AIAA-2002-1297, 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit AIAA Gossamer Spacecraft Forum, Denver, CO: April 22-25, 2002.
5. Cadogan, D., Smith, T., Uhelsky, F., Mackusick, M., "Morphing Inflatable Wing Development for Compact Package Unmanned Aerial Vehicles," AIAA No. AIAA-2004-1807, 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Palm Springs, CA, April 2004.
6. Cadogan, D.P., Scarborough S. E., "Rigidizable Materials for Use in Gossamer Space Inflatable Structures," AIAA-2001-1417, 42nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit AIAA Gossamer Spacecraft Forum, Seattle, WA: April 16-19, 2001.
7. Allred R., Hoyt, A., Harrah, L., McElroy, P., Scarborough, S., Cadogan, D., "Light Curing Rigidizable Inflatable Wing," AIAA-2004-1809, 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Palm Springs, CA, April 2004.
8. Hall D.,. "Airplane for Mars Exploration: Conceptual Design of the Full-Scale Vehicle; Design, Construction and Test of Performance and Deployment Models." Final Report, David Hall Consulting, May, 1997.
9. Smith, S.C., Hahn, A., Johnson, W., Kinnery, D., Pollitt, J., Reuther, J., "The Design of the Canyon Flyer, an Airplane for Mars Exploration." AIAA Paper 2000-0514, 38th AIAA Aerospace Sciences Meeting, Reno, NV, Jan. 2000.
10. Murray, J., Tartabini, P., "Development of a Mars Airplane Entry, Descent, and Flight Trajectory." NASA/TM-2001-209035, January, 2001.
11. Guynn, M., Croom, M., Smith, S., Parks, R., Gel-hausen, P., "Evolution of a Mars Airplane Concept for the ARES Mars Scout Mision." AIAA Paper 2003-6578, 2nd AIAA "Unmanned Unlimited" Systems, Technologies, and Operations Aerospace Conference, San Diego, CA, Sep., 2003.
12. Kearns, J., Usui, M., Smith, S., Scarborough, S., Smith, T., Cadogan, D., "Development of UV-Curable Inflatable Wings for Low Density Flight Applications," AIAA-2004-1503, 45th AIAA Gossamer Spacecraft Forum, Palm Springs, CA, April 2004.
13. Usui M., Jacob, J.D., Smith, S., Scarbor-ough, S., Cadogan, D., "Second Generation Inflat-able/Rigidizable Wings for Low-Density Applications," 46th AIAA Gossamer Spacecraft Forum, Austin, TX, April 2005.
14. Simpson, A.D., Usui, M., Smith, S.W., Jacob, J.D.,"Development and Flight Testing of a UAV with Inflatable-Rigidizable Wings," AIAA-2004-1373, 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2004.
15. Simpson, A.D., Usui, M., Smith, S., Jacob, J.D., "Aeromechanics of Inflatable Wings." AIAA 34th Fluid Dynamics Conference, Portland, OR, June, 2004.
16. Lissaman, P. B. S., "Low-Reynolds-Number Airfoils." Annual Review of Fluid Mechanics, 15, pp. 223-39, 1983.
17. Mueller, T., "Low Reynolds Number Aerodynamics." Springer Verlag, 1989.
18. Santhanakrishnan, A., Jacob, J. D., "Effect of Regular Surface Perturbations on Flow Over an Airfoil" AIAA-2005-5145, 35th AIAA Fluid Dynamics Conference and Exhibit, Toronto, Ontario, June 2005.
19. Simpson, A.D., Santhanakrishnan, A., Jacob, J.D., Smith, S., Lumpp J., Cadogan, D., "Flying on Air: UAV Flight Testing with Inflatable Wing Technology". AIAA-2004-6570 AIAA 3rd"Unmanned Unlimited" Technical Conference, Workshop and Exhibit, Chicago, Illinois, September 2004.
20. Kudva, J., Appa, K., Martin, C. A., Jardine, A. P., Sendeckyj, G., Harris, T., McGowan, A., Lake, R., "Design, Fabrication, and Testing of the DARPA/Wright Lab Smart Wing Wind Tunnel Model," Proceedings of the AIAA 38th Structures and Structural Dynamics Conference, Kissimmee, Florida, April 7-10, 1997,. AIAA Paper 97-1198.
21. Simpson, A.D., Coulombe, N., Jacob, J.D., Smith, S., "Morphing of Inflatable Wings," AIAA-2005-2110 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 13th AIAA/ASME/AHS Adaptive Structures Conference Austin, Texas, April 2005
22. Simpson, A.D., Jacob, J.D., "Aerodynamic Control of an Inflatable Wing Using Wing Warping." AIAA 35th Fluid Dynamics Conference, Toronto, Canada, June, 2005.
23. Kimberlin, R., Flight Testing of Fixed-Wing Aircraft, AIAA, Reston, 2003.
24. McCormick, B., Aerodynamics, Aeronautics, and Flight Mechanics, Wiley, New York, 1979.