NASA NTRS · 19690055470
Diffraction of shock wave by moving thin wing.
Abstract
Flow field pressure distribution due to plane shock wave impinging by thin wing moving in opposite direction, discussing mathematical formulation, analytic solution and applications
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Gunzburger, M., Ting, L.. 1969-06-01. Diffraction of shock wave by moving thin wing.. https://ntrs.nasa.gov/citations/19690055470
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