columbus · Pressure Measurements For Mach 8 Flows Over Expansion Corners And Ramps On An Internally Cooled Model. Part II. Flows Over A Flat Plate With And Without A Partial Span Ramp.

Pressure Measurements For Mach 8 Flows Over Expansion Corners And Ramps On An Internally Cooled Model. Part II. Flows Over A Flat Plate With And Without A Partial Span Ramp.

Title: Pressure Measurements For Mach 8 Flows Over Expansion Corners And Ramps On An Internally Cooled Model. Part II. Flows Over A Flat Plate With And Without A Partial Span Ramp.
Date: 1964
Index Abstract: Coming Soon
Photo Quality: Undetermined
Report Number: RTD TDR 63-4044 Part 2
Corporate Author: Grumman Aircraft Engineering Corp Bethpage N Y
Extent: 184
Identifier: AD0609458
Distribution Classification: 1
DTIC Record Exists: Yes
Distribution Change Authority Correspondence: None
Report Availability: Full text available by request
Date Issued: 1964-10
Abstract: The abstract for this report is either unavailable or has yet to be entered
Type: report
Provenance: Lockheed Martin Missiles & Fire Control
Creator: Kaufman, Louis G., II
Index In: USGRR Volume 40, Number 4 p. 38
Index Price: $5.00