columbus · Turbulent Boundary Layer Skin Friction, Heat Transfer and Pressure Measurements on Hypersonic Inlet Compression Surfaces

Turbulent Boundary Layer Skin Friction, Heat Transfer and Pressure Measurements on Hypersonic Inlet Compression Surfaces

Title: Turbulent Boundary Layer Skin Friction, Heat Transfer and Pressure Measurements on Hypersonic Inlet Compression Surfaces
Date: 1968
Index Abstract: Coming Soon
Photo Quality: Complete
Report Number: AFFDL TR 68-102
Corporate Author: Cornell Aeronautical Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Extent: 144
Identifier: AD0672836
Access Rights: OTS
Distribution Classification: 1
Contract: F33615-67-C-1203
DoD Project: 1366
DoD Task: None Given
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Report Availability: Full text available
Date Issued: 1968-07
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control
Type: report
Format: 1 online resource
Creator: Ryder, M. O., Jr.