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

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

By Marco A. S. Minucci

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Publish Date

1991

Publisher

American Institute of Aeronautics and Astronautics

Language

-

Pages

17

1-1 of 1 Editions

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

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

Pages: 17

Published In: 1991

Publisher: American Institute of Aeronautics and Astronautics