Transonic-buffet associated aeroelasticity of a supercritical wing
Author:
Affiliation:
1. Colorado, Univ., Boulder
2. NASA, Ames Research Center, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-286
Reference8 articles.
1. Eckstrom, C.V., Seidel, D.A., and Sanford, M.C. "Measurements of Unsteady Pressure and Structural Response for an Elastic SupercriticalWing,"NASATP3443, 1994.
2. Vortical flow computations on a flexible blended wing-body configuration
3. Unsteady aerodynamic and aeroelastic calculations for wings using Euler equations
4. An implicit finite-difference algorithm for hyperbolic systems in conservation-law form
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