An investigation of hypersonic shock tunnel testing at an equilibrium interface condition of 4,100K: theory and experiment
An edition of An investigation of hypersonic shock tunnel testing at an equilibrium interface condition of 4,100K: theory and experiment (1991)
By Marco A. S. Minucci
Publish Date
1991
Publisher
American Institute of Aeronautics and Astronautics
Language
-
Pages
17