Measurements of test time in the galcit 17-inch shock tube
Author:
Affiliation:
1. California Institute of Technology, Pasadena, Calif
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.2272
Reference15 articles.
1. HEAT TRANSFER TO A HEMISPHERE-CYLINDER AT LOW REYNOLDS NUMBERS
2. Blunt-Body Heat Transfer at Hypersonic Speed and Low Reynolds Numbers
3. Ferri, A and Zakkay, V , ' Measurements of stagnation point heat transfer at low Reynolds numbers," J Aerospace Sci 29, 847-850(1962)
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