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.

Investigation of Boundary Layer Transition in Hypersonic Flow at Angle of Attack

Report Number: AFFDL TR 66-122
Author: Nagel, A. L.
Author: Savage, R. T.
Author: Wanner, R.
Author: Blank, R. W.
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-08
Pages: 204
Contract: AF 33(615)-2011
Project: 1366
Task: 136606
AD Number: AD0803781

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


Provenance:
AFRL/VACA
Download this report

(PDF, 4.83 MB, 204 pages)

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