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Shock tube study of boundary layer instability

✍ Scribed by Raymond Brun; Pierre Auberger; Nguyen Van Qué


Book ID
111710828
Publisher
Elsevier Science
Year
1978
Tongue
English
Weight
310 KB
Volume
5
Category
Article
ISSN
0094-5765

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## Abstract Particle times of flight in incident shock flow were determined experimentally by marking several positions of the test gas (mainly Ar) in the shock tube with an infrared emitting gas (NO or CO~2~). From the local particle velocity, derived from the particle flight times, temperature an