Analytical aeroelastic characteristics of F-16 asymmetric external store configurations

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

Volumn 4, Issue , 2004, Pages 2665-2676

  Maxwell, Daniel L ^a,b   Dawson, Kenneth S ^a,b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b AFSEO   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BENDING (DEFORMATION); EIGENVALUES AND EIGENFUNCTIONS; FLIGHT DYNAMICS; FLUTTER (AERODYNAMICS); SUBSONIC AERODYNAMICS; VECTORS; VIBRATIONS (MECHANICAL); WINGS;

AEROELASTIC STABILITY; FLUTTER EXCITATION SYSTEMS (FES); MACH NUMBER; SUBSONIC FLUTTER;

AIRCRAFT;

EID: 16244399770     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-1755     Document Type: Conference Paper

References (5)

1. Denegri, Charles M., Jr., "Limit Cycle Oscillation Flight Test Results of a Fighter with External Stores," Journal of Aircraft, Vol 37, No 5, September-October 2000, pp. 761-769.
2. th AIAA Applied Aerodynamics Conference, June 1999. AIAA-99-3142.
3. Bunton, Robert W., and Denegri, Charles M., Jr., "Limit Cycle Oscillation Characteristics of Fighter Aircraft," Journal of Aircraft, Vol 37, No 5, September-October 2000, pp. 916-918.
4. th Structures, Structural Dynamics, and Materials Conference, AIAA-2003-1427, April 2003.
5. Rose, Ted, "A DMAP Alter to Calculate the Contributions of Individual Modes In a Modal Complex Eigenvalue or Frequency Response Solution", MSC America's Users Conference, 1998.