Pressure Distributions and Oil Film Photographs for Mach 5 Flows Past Fins Mounted on a Flat Plate: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Report Number: ASD TDR 63-755
Author: Kaufman, Louis G.
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Pages: 38
Contract: AF 33(616)-8130
Project: 8219
Task: 821902
AD Number: AD0422031
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: AFRL/VACA
