columbus · Pressure Measurements For Mach 8 Flows Over Expansion Corners And Ramps On An Internally Cooled Model. Part I. Expansion Corner Flows. Part Of An Investigation Of Hypersonic Flow Separation And Control Characteristics

Pressure Measurements For Mach 8 Flows Over Expansion Corners And Ramps On An Internally Cooled Model. Part I. Expansion Corner Flows. Part Of An Investigation Of Hypersonic Flow Separation And Control Characteristics

Title: Pressure Measurements For Mach 8 Flows Over Expansion Corners And Ramps On An Internally Cooled Model. Part I. Expansion Corner Flows. Part Of An Investigation Of Hypersonic Flow Separation And Control Characteristics
Date: 1963
Index Abstract: Coming Soon
Photo Quality: Incomplete
Report Number: RTD TDR 63-4044 Part 1
Corporate Author: Grumman Aircraft Engineering Corp Bethpage N Y
Laboratory: Air Force Flight Dynamics Laboratory
Extent: 73
Identifier: AD0431280
Access Rights: OTS
Distribution Classification: 1
Contract: AF 33(616)-8130
DoD Project: 8219
DoD Task: 821902
DTIC Record Exists: Yes
Distribution Change Authority Correspondence: None
Report Availability: Full text available by request
Date Issued: 1963-10
Abstract: The abstract for this report is either unavailable or has yet to be entered
Type: report
Provenance: AFRL/VACA; Bombardier/Aero; Lockheed Martin Missiles & Fire Control
Format: 73 pages ; 28 cm.
Creator: Kaufman, Louis G., II