Non-linear transonic flutter analysis for F-16 stores configuration clearance

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

Volumn 1, Issue , 2002, Pages 80-90

  Toth, Raymond G ^a   Canfield, Robert A ^a   Melville, Reid ^a  

^a Air Force Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

LIMIT CYCLE OSCILLATIONS (LCO);

COMPUTATIONAL FLUID DYNAMICS; NONLINEAR SYSTEMS; OSCILLATIONS; TRANSONIC AERODYNAMICS;

FLUTTER (AERODYNAMICS);

EID: 0036077896     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (22)

1. Limit cycle oscillation characteristics of fighter aircraft
2. Nonlinear simulation of F-16 aeroelastic instability
3. Limit cycle oscillation flight test results of a fighter with external stores
4. Physical mechanisms for limit-cycle oscillations of a cropped delta wing
5. Limit-cycle-oscillation studies of a fighter with external stores
6. Effects of angle of attack on nonlinear flutter of a delta wing
7. On the nonlinear structural damping mechanism of the wing/store limit cycle oscillation
8. Computational and experimental investigation of limit cycle oscillations in nonlinear aeroelastic systems
9. A methodology of large scale computational aeroelasticity for the MDA/MDO environment
10. Transonic flutter simulations using an implicit aeroelastic solver
11. Dynamic aeroelastic simulation of complex configurations using overset grid systems
12. Effect of store aerodynamics on wing/store flutter
13. Frequency domain unsteady transonic aerodynamics for flutter and limit cycle oscillation prediction
14. Energy based design and analysis of staggered solvers for nonlinear transient aeroelastic problems
15. F-16 Limit cycle oscillation testing with asymmetric stores
16. Correction of unsteady aerodynamic influence coefficients using experimental or CFD data
17. Improving the aerodynamic approximation in linear aeroelasticity