columbus · Pressure and Heat Transfer Measurements for Hypersonic Flows over Expansion Corners and Ahead of Ramps. Part IV: Mach 8 Heat Transfer Data for Flows Ahead of Ramps: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics

Pressure and Heat Transfer Measurements for Hypersonic Flows over Expansion Corners and Ahead of Ramps. Part IV: Mach 8 Heat Transfer Data for Flows Ahead of Ramps: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics

Title: Pressure and Heat Transfer Measurements for Hypersonic Flows over Expansion Corners and Ahead of Ramps. Part IV: Mach 8 Heat Transfer Data for Flows Ahead of Ramps: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Date: 1964
Index Abstract: Coming Soon
Photo Quality: Incomplete
Report Number: ASD TDR 63-679 Part 4
Creator: Kaufman, Louis G.
Corporate Author: Grumman Aircraft Engineering Coporation
Laboratory: Air Force Flight Dynamics Laboratory
Extent: 160
Identifier: AD0607038
Access Rights: OTS
Distribution Classification: 1
Contract: AF 33(616)-8130
DoD Project: 8219
DoD Task: 821902
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Report Availability: Full text available by request
Date Issued: 1964-07
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: AFRL/VACA; Lockheed Martin Missiles & Fire Control
Type: report