## 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
A numerical simulation of boundary layer effects in a shock tube
โ Scribed by K. J. Badcock
- Publisher
- John Wiley and Sons
- Year
- 1992
- Tongue
- English
- Weight
- 992 KB
- Volume
- 14
- Category
- Article
- ISSN
- 0271-2091
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