Aeroelastic analysis of modern complex wings

6th Symposium on Multidisciplinary Analysis and Optimization

Volumn , Issue , 1996, Pages 258-265

  Kapania, Rakesh K ^a   Bhardwaj, Manoj K ^a   Reichenbach, Eric ^b   Guruswamy, Guru P ^c  

^a VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^b BOEING COMPANY   (United States)

^c NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; BOMBERS; CODES (SYMBOLS); COMPUTATIONAL FLUID DYNAMICS; NASA; STRUCTURAL DYNAMICS; SUPERSONIC AIRCRAFT;

AEROELASTIC ANALYSIS; AMES RESEARCH CENTERS; CFD CODES; COMPUTATIONAL FLUID DYNAMICS CODES; COMPUTATIONAL STRUCTURAL DYNAMICS; MCDONNELL DOUGLAS; SUPERCRITICAL; WING BOX;

WINGS;

EID: 84982318254     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-4011     Document Type: Conference Paper

References (10)

1. Guruswamy, G.P. and Yang, T.Y., “Aeroelastic Time-Response Analysis of Thin Airfoils by Transonic Code LTRAN2”, Computers and Fluids, Vol. 9, No. 4, Dec. 1980, pp. 409-425.
2. Macmurdy, D.E., Guruswamy, G.P., and Kapania, R.K., “Static Aeroelastic Analysis of Wings Using Euler/Navier-Stokes Equations Coupled with Improved Wing-Box Finite Element Structures”, AIAA Paper 94-1587, April 1994.
3. Bhardwaj, M.K., Kapania, R.K., Byun, C., and Guruswamy, G.P., “Parallel Aeroelastic Computations By Using Coupled Euler Flow and Wing-Box Structural Models”, AIAA Paper 95-1291, April 1995.
4. Byun, C. and Guruswamy, G.P., “Wing-Body Aeroelasticity Using Finite-Difference Fluid/Finite Element Structural Equations on Parallel Computers”, AIAA Paper 94-1487, April 1994.
5. Harder, R.L. and Desmarais, R.N., “Interpolation Using Surface Splines”, Journal of Aircraft, Vol. 9, No. 2, October 1971, pp. 189-191.
6. Guruswamy, G.P., “Coupled Finite- Difference/Finite Element Approach for Wing-Body Aeroelasticity”, AIAA Paper 92-4680, Sep. 1992.
7. Guruswamy, G.P. and Byun, C., “Fluid-Structural Interactions Using Navier-Stokes Flow Equations Coupled with Shell Finite Element Structures”, AIAA Paper 93-3087, July 1993.
8. Sanford, Maynard C., Seidel, David A., Eckstrom, Clinton V., and Spain, Charles V., “Geometrical and Structural Properties of an Aeroelastic Research Wing (ARW-2)”, NASA TM 4110, April 1989.
9. Allman, D.J., “A Compatible Triangular Element Including Vertex Rotations for Plane Elasticity Problems”, Computers and Structures, Vol. 19, No. 12, 1984, pp. 1-8.
10. Farhat, C. and Wilson, E., “A Parallel Active Column Equation Solver”, Computers and Structures, Vol. 28, No.2, 1988, pp. 289-304.