columbus · Pressure Measurements for Mach 8 Flows Over Expansion Corners and Ramps on an Internally Cooled Model Part III. Flows Over Full Span Ramps Mounted on a Flat Plate

Pressure Measurements for Mach 8 Flows Over Expansion Corners and Ramps on an Internally Cooled Model Part III. Flows Over Full Span Ramps Mounted on a Flat Plate

Title: Pressure Measurements for Mach 8 Flows Over Expansion Corners and Ramps on an Internally Cooled Model Part III. Flows Over Full Span Ramps Mounted on a Flat Plate
Date: 1964
Index Abstract: Not Available
Photo Quality: Complete
Report Number: RTD TDR 63-4044 Part 3
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Extent: 158
Identifier: AD0601805
Access Rights: OTS
Distribution Classification: 1
Contract: AF 33(616)-8130
DoD Project: 8219
DoD Task: 821902
DTIC Record Exists: No
Distribution Conflict: No
Report Availability: Full text available
Date Issued: 1964-05
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Bombardier/Aero
Type: report
Format: 1 online resource
Creator: Kaufman, Louis G., II