NASA NTRS · 19960022429
Computation Of Flow About A Pitching Wing/Fuselage
Abstract
Report presents computational study of unsteady transonic flow about airplanelike body as body pitches upward in increasing angle of attack.
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Obayashi, S., Guruswamy, G. P., Tu, E. L.. 1996-05-01. Computation Of Flow About A Pitching Wing/Fuselage. https://ntrs.nasa.gov/citations/19960022429
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