NASA NTRS · 19710018896
Uniform approximations for shocks generated by thin nonlifting rectangular wings
Abstract
Flow field approximation for sonic boom shock wave generation by thin nonlifting rectangular wing
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Davis, S. S., Friedman, M. B.. 1971-01-01. Uniform approximations for shocks generated by thin nonlifting rectangular wings. https://ntrs.nasa.gov/citations/19710018896
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