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Acoustical Methods in Supersonic Aerodynamics

✍ Scribed by Miles, John W.

Book ID
118016090
Publisher
American Institute of Physics
Year
1948
Tongue
English
Weight
924 KB
Volume
20
Category
Article
ISSN
0001-4966

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## Abstract A finite element method to determine unsteady aerodynamic influence coefficients, consistent with the stiffness and inertia properties of a lifting surface in supersonic flow, is described. This is basically a kinematic method, which reduces the dynamical equations of a non‐conservative