An Improved Mach-Box Approach for Supersonic Oscillatory Pressures
Author:
Affiliation:
1. Grumman Aerospace Corporation, Bethpage, N. Y.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.58869
Reference18 articles.
1. Aerodynamic Flutter Derivatives for a Flexible Wing with Supersonic and Subsonic Edges
2. Oscillatory supersonic kernel function method for interfering surfaces
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1. Flutter analysis of hybrid metal-composite low aspect ratio trapezoidal wings in supersonic flow;Chinese Journal of Aeronautics;2017-02
2. NONPLANAR DOUBLET-POINT METHOD FOR SUPERSONIC UNSTEADY AERODYNAMICS;34th Structures, Structural Dynamics and Materials Conference;1993-04-19
3. Oscillating wings and bodies with flexure in supersonic flow;Journal of Aircraft;1988-06
4. Subsonic/supersonic linear unsteady analysis;3rd Applied Aerodynamics Conference;1985-08-17
5. Doublet-Point Method for Supersonic Unsteady Lifting Surfaces.;AIAA Journal;1984-02
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