Abstract
An aeroelastic package consisting of 1) an aerodynamic solver, 2) a structural response model, and 3) a grid generation/update program has been developed to study both static and dynamic response of flexible aerospace configurations. The aerodynamics at present is a full potential solver but can be an Euler/Navier-Stokes solver also. The structural response is based on a generalized modal representation. The grid generation package not only sets up the initial grid, but also updates the grid position in time to follow the instantaneous position of a flexible configuration using a “grid speed” procedure.
The aeroelastic package can handle 1) static rigid, 2) dynamic rigid, 3) static flexible, and 4) dynamic flexible cases. Also, the aerodynamic solver is based on an unsteady formulation and can handle subsonic, transonic, and supersonic flow conditions. Results are presented for rigid and flexible configurations at different Mach numbers ranging from subsonic to supersonic conditions. The dynamic response of a flexible wing below and above its flutter point is demonstrated.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
G.P. Guruswamy. Transonic aeroelasticity of wings with active control surfaces. Paper No. 87–0709, ASME 28th Structures, Structural Dynamics and Materials Conference, Monterey, CA, April, 1987, pp. 16–30.
C.J. Borland, R.G. Thorne, and L.R. Yeagley. Transonic unsteady aerodynamics for aeroelastic applications. Vol. 1, AFWAL-TR-80–3107, May, 1981.
J.B. Malone, N.L. Sankar, and W.A. Sotomayer. Unsteady aerodynamic modeling of a fighter wing in transonic flow. AIAA Paper No. 84–1566, AIAA 17th Fluid Dynamics, Plasmadynamics, and Lasers Conference, June 25–27, 1984.
V. Shankar, H. Ide, J. Gorski, and S. Osher. A fast, time-accurate unsteady full potential scheme. AIAA Paper No. 85–1512-CP, AIAA 6th Computational Fluid Dynamics Conference, Cincinnati, July 15–17, 1985.
V. Shankar and H. Ide. Aeroelastic computations of flexible configurations. Symposium on Advances and Trends in Computational Structural Mechanics and Fluid Dynamics, Washington, D.C., October 17–19, 1988.
V. Shankar, H. Ide, and T. Goebel. Unsteady full potential computations for complex configurations. AIAA Paper No. 87–0110, AIAA 25th Aerospace Sciences Meeting, Reno, Nevada, January 12–15, 1987.
H. Ide and V. Shankar. Unsteady full potential aeroelastic computations for flexible configurations. AIAA Paper No. 87–1238, AIAA 19th Fluid Dynamics, Plasmadynamics, and Lasers Conference, Hawaii, June 8–10, 1987.
G.D. Miller and T.R. Logan. AFW technology wind tunnel test results from first tunnel entry. Rockwell Report NA/86/1399L, AFWAL Contract F33615–85-C3209, CDRL 007, February, 1987.
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 1989 Springer-Verlag Berlin Heidelberg
About this paper
Cite this paper
Shankar, V., Ide, H. (1989). Unsteady Aeroelastic Computations for Flexible Configurations at Transonic and Supersonic Speeds. In: Zierep, J., Oertel, H. (eds) Symposium Transsonicum III. International Union of Theoretical and Applied Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-83584-1_37
Download citation
DOI: https://doi.org/10.1007/978-3-642-83584-1_37
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-83586-5
Online ISBN: 978-3-642-83584-1
eBook Packages: Springer Book Archive