Hypersonic aerodynamic/aerothermodynamic testing capabilities at Langley Research Center

Publisher Website

6 July 1992

conference paper
Published by American Institute of Aeronautics and Astronautics (AIAA)

https://doi.org/10.2514/6.1992-3937

Abstract

No abstract available

This publication has 2 references indexed in Scilit:

Langley 20-inch hypersonic CF4 tunnel - A facility for simulating real-gas effects
Published by American Institute of Aeronautics and Astronautics (AIAA) ,1992
Reduction of data from thin-film heat-transfer gages - A concise numerical technique.
AIAA Journal, 1966