Box 2
Container
Contains 1 Collection or Record:
Vahl, W. A.; Weidner, J. P. A Preliminary Assessment of the Impact of 2-D Exhaust-Nozzle Geometry on the Cruise Range of a Hypersonic Aircraft With Top-Mounted Ramjet Propulsion. NASA TM -81841. NASA Scientific and Technical Information Branch, 1980
Item — Box: 2, Item: 16
Identifier: MSA 312, Series 2, Item 16
Scope and Contents
From the Series:
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Dates:
1980