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)

An investigation of hypersonic shock tunnel testing at an equilibrium interface condition of 4,100K: theory and experiment

By Marco A. S. Minucci

0 (0 Ratings)

0 Want to read0 Currently reading0 Have read

Publish Date

1991

Publisher

American Institute of Aeronautics and Astronautics

Language

Pages

Description:

subjects: Hypersonic flow, Hypersonic shock tubes