F/A-18E/F aeroservoelastic design, analysis, and test

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

Volumn 6, Issue , 2003, Pages 4383-4392

  Pitt, Dale M ^a   Hayes, William B ^a   Goodman, Charles E ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; BENDING STRENGTH; COMPUTER CONTROL SYSTEMS; COMPUTER SIMULATION; FLIGHT DYNAMICS; STIFFNESS; SYSTEMS ANALYSIS; WIND TUNNELS; WINGS;

AEROSERVOELASTIC TESTING; AEROSERVOELASTICITY; FLIGHT CONTROL SYSTEM; TORSIONAL STIFFNESS;

AERODYNAMICS;

EID: 0043011412     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

1. Anonymous, "F/A-18E/F Flight Control System Design Report Volume II - Control Law Operation and Mechanization", McDonnell Douglas report MDC 95A0037, 31 July 1995.
2. Eversman, W., and Pitt, D.M., "A Hybrid Doublet Lattice - Doublet Point Method for General Lifting Surface Configurations in Subsonic Flow", AIAA Paper 89-1322 Presented at the AIAA/ASME/AHS/ASCE 28th Structures, Structural Dynamics, and Materials Conference, 3 April 1989, Mobile, Alabama.
3. Pitt, D.M., and Goodman, C. E., "FAMUSS: A New Aeroservoelastic Modeling Tool", AIAA Paper 92-2395, Presented at the 33rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 13-15 April 1992.
4. Goodman, C.E., "Flexible Aircraft Modeling Using State Space (FAMUSS) Version 3.2, McDonnell Douglas Report MDC 94P0047, 16 Dec 1994.
5. Goodman, C. E., "Accurate Subcritical Damping Solution of Flutter Equation Using Piecewise Aerodynamic Function", Journal of Aircraft, Volume 38, Number 4, pages 755-763, July-August 2001
6. Halley, I.A., Schwartz, J.D., F/A-18E/F Design Flutter and Divergence Analysis Report - Volume IV - Aeroservoelasticity, McDonnell Douglas Report MDC 95A0093, 31 August 1995.
7. Cheng, P., Hirner, T., Aircraft Aeroservoelastic Compensation Using Constrained Optimization, 33rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, April 13-15, 1992, Dallas, Texas
8. Cheng, P., Hirner, T., Automated Procedure For Aircraft Aeroservoelastic Compensation, AIAA-92-4606, AIAA Guidance, Navigation, and Control Conference, August 10-12, 1992, Hilton Head Island, South Carolina.
9. Weichelt G.A., Sibbitt B.C., Pitt D.M., F/A-18 E1 Correlation and Divergence Analysis Report - Clean Wing - Volume II - Aeroservoelasticity, McDonnell Douglas Report MDC 95A0157, 22 July 1996.
10. Sherman, S.T., Weichelt, G.A., F/A-18 E1 Clean Wing Ground Vibration Test Report Volume II - Structural Mode Interaction, McDonnell Douglas Report MDC 95A0156, 1 Feb 1996.