Experimental results from the active aeroelastic wing wind tunnel test program

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 8, Issue , 2005, Pages 5384-5399

  Heeg, Jennifer ^a,e,f   Spain, Charles V ^a,e   Florence, James R ^a,e   Wieseman, Carol D ^a,e   Ivanco, Thomas G ^a,e,f   DeMoss, Joshua A ^a,e,f   Silva, Walter A ^a,e,f   Panetta, Andrew ^b,f,g   Lively, Peter ^c,f,g   Tumwa, Vic ^d,e,h,i  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NORTHROP GRUMMAN CORPORATION   (United States)

^c LOCKHEED MARTIN   (United States)

^d Jacobs Sverdrup   (United States)

^e Aeroelasticity Branch   (United States)

^f AIAA   (United States)

^g VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^h Mail Stop 230 ^*  (United States)

ⁱ Mail Stop 340   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT; EQUIPMENT TESTING; FLIGHT DYNAMICS; WIND TUNNELS;

ACTIVE AEROELASTIC WING (AAW); AEROELASTIC MODEL; SCALING LAWS; WIND TUNNEL TESTING;

AEROSPACE ENGINEERING;

EID: 28844477969     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-2234     Document Type: Conference Paper

References (15)

1. th Von Karman Lecture, AIAA Journal of Aircraft, Vol 13, No 9, September 1976.
2. F/A-18 Stability and Control Data Report. Volume I: Low Angle of Attack. MDC 7247. Issued August 31, 1981, revised November 15, 1982.
3. F/A-18 Aerodynamic Stability and Control and Flying Qualities Report. Volume I: Stability and Control Data. MDC 3957, Issued June 1, 1976, revised March 16. 1981.
4. Perry, B. III, Cole, S.R., and Miller, G.D., ''Summary of an active flexible wing program,'' AIAA Journal of Aircraft, Vol 32, No 1, January-February 1995.
5. Pendleton, E. W., Besserte, D., Field, P.B., Miller, G. D., and Griffin, K.E., "Active aeroelastic wing flight research program and model analytical development," AIAA Journal of Aircraft, Vol 37, No. 4, July-August 2000.
6. Abel, I. "Evaluation of a technology for determining airplane aileron effectiveness and roll rate by using a static aeroelastically scaled model", NASA TN D5538, November 1969.
7. th AIAA/ASME/ASCE/AHS. ASC Structures, Structural Dynamics and Materials Conference, April, 2004, Palm Springs, California.
8. Molyneux, W.G., "Aeroelastic modeling," RAE Technical note number Structures 353, March 1964.
9. Burner, A.W. and Liu, T., "Videogrammetric Model Deformation Measurement Technique," AIAA Journal of Aircraft, Vol 38, No 4, July 2001
10. th AIAA/ASME/ASCE/AHS.ASC Structures, Structural Dynamics and Materials Conference, April, 2004, Palm Springs, California
11. th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, April, 2005, Austin, Texas
12. Rodden, William P., and Erwin J. Johnson. MSC/NASTRAN Aeroelastic Analysis User's Guide. Version 68, 1994.
13. Rodden, W. P., Giesing, J.P., and Kalman, T. P., "New Developments and Applications of the Subsonic Doublet-Lattice Method for Nonplanar Configurations," AGARD Symposium on Unsteady Aerodynamics for Aeroelastic Analyses of Interfering Surfaces, Paper number 4, November 1970.
14. Chen, P.C, and Liu, D.D., "A Harmonic Gradient Method for Unsteady Supersonic Flow Calculations," Journal of Aircraft, Vol. 22, No. 5, May 1985.
15. Roskam, J. "Airplane flight dynamics and automatic flight controls, part I," pp 71-81, Roskam Aviation and Engineering Corporation 1979.