Contrails
The goal of the Contrails project is to help preserve and disseminate the technical record of 20th century aerospace research, highlighting in particular the research endeavors of the Illinois Tech community.

Pressure and Heat Transfer Measurements for Hypersonic Flows over Expansion Corners and Ahead of Ramps Part II: Mach 5 Pressure Data for Flows Ahead of Ramps: :Part of an Investigation of Hypersonic Flow Separation and Control Characteristics

Report Number: ASD TDR 63-679 Part 2
Author: Kaufman, Louis G.
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Pages: 227
Contract: AF 33(616)-8130
Project: 8219
Task: 821902
AD Number: AD0421859

Abstract:
The abstract for this report is either unavailable or has yet to be entered


Provenance:
AFRL/VACA
This report has yet to be scanned by Contrails staff

Request scanning of this report

Other options for obtaining this report

Via the Defense Technical Information Center (DTIC):
A record for this report, and possibly a full-image download of the report, exists at DTIC

Via National Technical Information Service:
This report may have been digitized and made freely available for public download, or made publicly available for purchase by the National Technical Information Service through their online database, the National Technical Reports Library

Indications of Public Availability
No digital image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement