F-22 aeroelastic design and test validation

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

Volumn 1, Issue , 2007, Pages 718-738

  Anderson, William D ^a,c,d   Mortara, Sean ^b,e  

^a LOCKHEED MARTIN   (United States)

^b WRIGHT PATTERSON AIR FORCE BASE   (United States)

^c F 22 Structures IPT ^*  (United States)

^d AIAA   (United States)

^e Airframe Structures   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTIC ANALYSIS; FLIGHT VERIFICATION; MANUFACTURING DEVELOPMENT;

AERODYNAMICS; OPTIMIZATION; PARAMETER ESTIMATION; PRODUCT DEVELOPMENT; STRUCTURAL ANALYSIS;

AEROSPACE ENGINEERING;

EID: 34547519962     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

1. Aircraft Structural Integrity Program, MIL-STD-1530A.
2. Aircraft Structures, General Specification for, AFGS-87221 A, 8 June 1990.
3. F-22 Air Vehicle Structural Design Criteria Report, F-22 Program Report 5PPYA005K, May 2005.
4. Hassig, H. J., "An Approximate True Damping Solution of the Flutter Equation by Determinant Iteration", Journal of Aircraft, Vol 8, No. 11, November 1971, pp. 885-889.
5. Kalman, T. P., Rodden, W. P., and Giesing, J. P., "Application of Doublet Lattice Method to Nonplanar Configurations in Subsonic Flow", Journal of Aircraft, Vol. 8 No. 6, June 1971, pp. 406-413.
6. Chen, P. C., and Liu, D. D., "Harmonic Gradient Method for Unsteady Supersonic Flow Calculations", Journal of Aircraft, Vol. 22, No. 5, May 1985.
7. Guruswamy, G. P., and Byun, C., "Fluid-Structural Interactions Using Navier-Stokes Flow Equations Coupled with Shell Finite Element Structures", AIAA-93-3087.
8. Radovcich, N. A., and Layton, D. A., "The F-22 Structural/ Aeroelastic Design Process with MDO Examples", AIAA-1998-4732.
9. th ed., Dover Publications Inc., Mineola, NY, 1985, Chap. 8.
10. th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2007 (to be published).
11. th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2007 (to be published).
12. Davis, R. A., RT-DAS User's Guide, Lockheed Martin Document 73HA-006-99, Marietta, GA, January 1999.
13. Cole, H. A., Jr., "On-Line Failure and Damping Measurement of Aerospace Structures by Random Decrement Signatures", NASA CR 2205, Washington, D. C., March 1973.