An Experimental and Analytical Investigation of Hypersonic Inlet Boundary Layers

Download this report (PDF, 8.66 MB, 407 pages)
Report Number: AFFDL TR 65-123 Volume 2
Author(s): Stroud, J. F., Miller, L. D.
Corporate Author(s): Lockheed-California Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-08
Pages: 407
Contract: AF 33(657)-8833
DoD Project: 1366
DoD Task: 136605
Identifier: AD0621344

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

Provenance: Lockheed Martin Missiles & Fire Control

Other options for obtaining this report:

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

Via National Technical Report Library:
The NTRL Order Number for this report is: AD621344
A record for this report, and possibly a pdf download of the report, exists at NTRL

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



Export