Efficient aeroelastic analysis using computational unsteady aerodynamics

Journal of Aircraft

Volumn 38, Issue 3, 2001, Pages 547-556

  Raveh, D E ^a   Levy, Y ^b   Karpel, M ^b  

^a GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

^b TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; BOUNDARY CONDITIONS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; NAVIER STOKES EQUATIONS; TRANSONIC FLOW; UNSTEADY FLOW; WINGS;

COMPUTATIONAL UNSTEADY AERODYNAMICS; GENERALIZED AERODYNAMIC FORCES; MACH NUMBER;

FLUTTER (AERODYNAMICS);

EID: 0035334167     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2795     Document Type: Article

References (22)

1. Reduced order models in unsteady aerodynamics
2. Reduced-order models based on linear and nonlinear aerodynamic impulse response
3. Accelerating CFD-based aeroelastic predictions using system identification
4. Development of discrete-time aerodynamic model for CFD-based aeroelastic analysis
5. Application of nonlinear systems theory to transonic unsteady aerodynamic responses
6. Extension of a nonlinear system theory to general-frequency unsteady transonic aerodynamic responses
7. Identification of linear and nonlinear aerodynamic impulse response using digital filter techniques
8. Discrete-time linear and nonlinear aerodynamic impulse responses for efficient CFD analyses
9. Computation of unsteady transonic flows by indicial methods
10. AGARD standard aeroelastic configurations for dynamic response, candidate configuration I.- Wing 445.6
11. CFL3D user's manual (Version 5.0)
12. Structural optimization of flight vehicles with computational-fluid-dynamics-based maneuver loads
13. Integrated aero-structural design of maneuvering flexible flight vehicles
14. A damping perturbation method for flutter solution: The g-method
15. Modern wing flutter analysis by computational fluid dynamics method
16. Wing flutter boundary prediction using unsteady Euler aerodynamic method
17. Wing flutter computations using an aerodynamic model based on the Navier-Stokes equations
18. Structural optimization using computational aerodynamics
19. Mach number effects on transonic aeroelastic forces and flutter characteristics