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

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

Title: 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
Date: 1962
Index Abstract: Limited
Photo Quality: Incomplete
Report Number: ASD TDR 62-155 Part 2
Creator: Mazelsky, Bernard; Amey, Harry B., Jr.
Corporate Author: Aeroject-General Corporation
Laboratory: Flight Dynamics Laboratory
Extent: 17
Identifier: AD0292624
Access Rights: NA
Distribution Classification: 2
Contract: AF 33(616)-7420
DoD Project: 1370
DoD Task: 137003
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Report Availability: Not available via Contrails
Date Issued: 1962-11
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: AFRL/VACA
Type: report