Development and application of an integrated multidisciplinary analysis capability

International Journal for Numerical Methods in Engineering

Volumn 40, Issue 3, 1997, Pages 533-550

  Gupta, K K ^a  

^a NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

Author keywords

Aeroelasticity; Aeroservoelasticity; FEM; Multidisciplinary analysis

Indexed keywords

AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SOFTWARE; DAMPING; EQUATIONS OF MOTION; FEEDBACK CONTROL; FINITE ELEMENT METHOD; FREQUENCY RESPONSE; LAPLACE TRANSFORMS; MATRIX ALGEBRA; STATE SPACE METHODS; STRUCTURAL ANALYSIS;

AEROSERVOELASTIC ANALYSIS; MULTIDISCIPLINARY ANALYSIS; UNSTEADY AERODYNAMIC FORCES;

NUMERICAL METHODS;

EID: 0031078309     PISSN: 00295981     EISSN: None     Source Type: Journal    
DOI: 10.1002/(SICI)1097-0207(19970215)40:3<533::AID-NME78>3.0.CO;2-W     Document Type: Article

References (20)

1. R. F. Taylor, K. L. Miller and R. A. Brockman, 'A procedure for flutter analysis of FASTOP-3 compatible mathematical models, volume I -theory and application', AFWAL-TR8I-3063, 1981.
2. I. Abel, 'An analytical technique for predicting the characteristics of a flexible wing equipped with an active flutter-suppression system and comparison with wind-tunnel data', NASA TP-1367, 1979.
3. K. K. Gupta, M. J. Brenner and L. S. Voelker, 'Development of an integrated aeroservoelastic analysis program and correlation with test data', NASA TP-3120, 1991.
4. E. M. Lee-Rausch and J. T. Batina, 'Wing flutter boundary prediction using unsteady euler aerodynamic method', NASA TM-107732, 1993.
5. R. D. Rausch, J. T. Batina and H. T. Y. Yang, Three-dimensional time-marching aeroelastic analyses using an unstructured-grid Euler method', A1AA J., 31, 1626-1633 (1993).
6. K. K. Gupta, 'STARS- an integrated general-purpose finite element structural, aeroelastic, and aeroservoelastic analysis computer program', NASA TM-101709, 1990 (Revised May, 1995).
7. R F. Whitbcck, D. G. J. Didaleusky and L. G. Hofman, 'Frequency response of digitally controlled systems', J. Guidance Control 4, 423-427 (1981).
8. J. Donea, 'A Taylor-Galerkin method for convective transport problems'. Int. j. numer. methods eng., 20, 101-119 (1984).
9. J Peraire, J. Peiro, L. Formaggia, K. Morgan and O. C. Zienkiewicz, 'Finite element Euler computations in three dimensions', Int. j. numer. methods eng.. 26, 2135-2159 (1988).
10. K. K. Gupta and K. L. Petersen. 'Multidisciplinary aeroelastic analysis of a generic hypersonic vehicle', NASA TM-4544, 1993.
11. J Peraire, J. Peiro and K. Morgan. 'A 3-D finite element multigrid solver for the Euler equations', AIAA Paper 92-0449, 1992.
12. J. Heeg, T. Zeiler, A. Pototzky, V. Spain and W. Engelund, 'Aerothermoelastic analysis of a NASP demonstrator model', AIAA Paper 93-1366. 1993
13. W. J Sefic and C. M. Maxwell, 'X-29A technology demonstrator flight test program overview', NASA TP-86809,1986.
14. K. K. Gupta, M. J. Brenner and L S. Voelker, 'Integrated aeroservoelastic analysis capability with X-29A comparisons', J. Aircraft, 26, 84-90 (1989).
15. J. M. Brenner, 'Aeroservoelastic modeling and validation of a thrust vectoring F-I8', NASA TP-3645, 1996.
16. J. M. Brenner, 'Actuator and aerodynamic modeling for high-angle-of-attack aeroservoclasticity', NASA TM-4493, 1993
17. E C Yates, Jr., N. S. Land and J T. Foughner, Jr., 'Measured and calculated subsonic and transonic flutter characteristics of a 45° sweptback wing planform in air and in Freon-12 in the Langley transonic dynamics tunnel', NASA TN D-1616. 1963.
18. E C. Yates, Jr., 'AGARD standard aeroelastic configuration for dynamic response, candidate configuration 1.-Wing 445.6', NASA TM-100492, 1987.
19. C. V. Spain, D. L. Soistmann and T. W. Linville, 'Integration of thermal effects into finite element aerothermoelastic analysis with illustrative results'. NASA CR-1059, 1989.
20. H. J. Dunn, 'UNAERO: a package of FORTRAN subroutines for approximating unsteady aerodynamics in the time domain', NASA TM-86392, 1985.