Report presents computational study of unsteady transonic flow about airplanelike body as body pitches upward in increasing angle of attack.
Computation Of Flow About A Pitching Wing/Fuselage
NASA Tech Briefs ; 20 , 5
1996-05-01
Miscellaneous
No indication
English
Computation of Flow About a Pitching Wing-Fuselage
Online Contents | 1996
Algebraic grid generation about wing-fuselage bodies
NTRS | 1987
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