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Lift, Pitching-Moment, and Rolling-Moment Coefficients on Planar, Twisted, and Cambered Wings and Flaps for a 70 Degree Delta Wing: Part Two - Transonic Flow

Report Number: ASD TDR 62-155 Part 2
Author: Mazelsky, Bernard
Author: Amey, Harry B., Jr.
Corporate Author: Aeroject-General Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-11
Pages: 17
Contract: AF 33(616)-7420
Project: 1370
Task: 137003
AD Number: AD0292624

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