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
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Report Number: ASD TDR 62-155 Part 2
Author(s): Mazelsky, Bernard, Amey, Harry B., Jr.
Corporate Author(s): Aeroject-General Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-11
Pages: 17
Contract: AF 33(616)-7420
DoD Project: 1370
DoD Task: 137003
Identifier: AD0292624
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: AFRL/VACA
Author(s): Mazelsky, Bernard, Amey, Harry B., Jr.
Corporate Author(s): Aeroject-General Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-11
Pages: 17
Contract: AF 33(616)-7420
DoD Project: 1370
DoD Task: 137003
Identifier: AD0292624
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: AFRL/VACA