columbus · Theoretical Prediction of Pressures in Hypersonic Flow with Special Referencce to Configurations Having Attached Leading Edges Shock: Part II. Experimental Pressure Measurements at Mach 5 and 8

Theoretical Prediction of Pressures in Hypersonic Flow with Special Referencce to Configurations Having Attached Leading Edges Shock: Part II. Experimental Pressure Measurements at Mach 5 and 8

Title: Theoretical Prediction of Pressures in Hypersonic Flow with Special Referencce to Configurations Having Attached Leading Edges Shock: Part II. Experimental Pressure Measurements at Mach 5 and 8
Date: 1962
Index Abstract: Limited
Photo Quality: Incomplete
Report Number: ASD TR 61-60 Part 2
Creator: Mead, Harold R.; Koch, Frank
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Extent: 169
Identifier: AD0282301
Access Rights: NA
Distribution Classification: 2
Contract: AF 33(616)-6400
DoD Project: 8219
DoD Task: 82159
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Report Availability: Not available via Contrails
Date Issued: 1962-05
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: AFRL/VACA
Type: report