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Solution of the problem of a wing oscillation in a supersonic gas flow
T. P. Arsent'ev,
R. G. Barantsev Saint-Petersburg State University
Abstract:
The problem of a thin wing oscillation in a supersonic flow that was formulated in [1] is solved for all frequency
intervals.
Key words:
thin wing oscillation, supersonic gas flow, analytical solution, asymptotics for small and large frequencies.
UDC:
553.6.011,
519.6 Received: 20.11.2007
© , 2024
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