A review of numerical fluids/structures interface methods for computations using high-fidelity equations

Computers and Structures

Volumn 80, Issue 1, 2002, Pages 31-41

  Guruswamy, Guru P ^a  

^a NASA AMES RESEARCH CENTER   (United States)

Author keywords

Aeroelasticity; Computers; Finite elements; High fidelity; Navier Stokes

Indexed keywords

AEROSPACE APPLICATIONS; FINITE ELEMENT METHOD; FLUID STRUCTURE INTERACTION; NAVIER STOKES EQUATIONS;

HIGH-FIDELITY EQUATIONS;

COMPUTATIONAL FLUID DYNAMICS;

EID: 0036137723     PISSN: 00457949     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0045-7949(01)00164-X     Document Type: Article

References (37)

1. Self-induced oscillation wind tunnel test of a variable sweep wing
2. Navier-Stokes computations, including a complete F-16 aircraft
3. Aeroelastic time response analysis of thin airfoils by transonic code LTRAN2
4. ATRAN3S - An unsteady transonic code for clean wings
5. Recent advances in transonic computational aeroelasticity
6. Unsteady aerodynamic and aeroelastic calculations of wings using Euler equations
7. Vortical flow computations on a flexible blended wing-body configuration
8. ENSAERO - A multidisciplinary program for fluid/structural interaction studies of aerospace vehicles
9. Close-range photo-grammetric measurement of static deflections for an aeroelastic supercritical wing
10. Transonic-buffet associated aeroelasticity of a supercritical wing
11. Static aeroelastic analysis of fighter aircraft using a three-dimensional Navier-Stokes algorithm
12. A computational fluid dynamics/computational structural dynamics interaction methodology for aircraft wings
13. Coupled finite-difference/finite-element approach for wing-body aeroelasticity
14. Aeroelastic analysis of transonic wings using Navier-Stokes equations and a nonlinear beam model
15. Finite-surface spline
16. Interpolation using surface spline
17. The determination of load and slope transformation matrices for aeroelastic analysis
18. Structural and aerodynamic data transformation using inverse isoparametric mapping
19. Numerical inverse isoparametric mapping in remeshing and nodal quantity contouring
20. Wing-body aeroelasticity on parallel computers
21. Interfacing of fluids and structural models via innovative structural boundary element method
22. A unified aeroelastic surface formulation
23. A general method for calculating aero-structure interaction on aircraft configuration
24. An experimental investigation of aerodynamics effects of airfoil thickness on transonic flutter characteristics
25. Fluid-structural interactions using Navier-Stokes flow equations with shell finite-element structures
26. The inf-sup condition and its evaluation for mixed finite element methods
27. Aeroelastic analysis of wings using Euler/Navier-Stokes equations coupled with improved wing-box finite element structures
28. Displacement extrapolations for CFD+CSM Aeroelastic analysis
29. High fidelity analysis into parallel multidisciplinary aircraft analysis