THE FREE-MOLECULE IMPACT-PRESSURE PROBE OF ARBITRARY LENGTH
Author:
Affiliation:
1. Institute of Aerophysics, University of Toronto,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.1503
Reference12 articles.
1. Courant, R., and Friedrichs, K. O., Supersonic Flow and Shock Waves, p.199, Interscience Publishers, Inc., New York, 1948.
2. A Note on One-Dimensional Hydromagnetic Flow With Transverse Magnetic Field
3. A Note on Hydromagnetic Simple-Wave Flow
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