Measurement of droplet size for wide range particle distributions
Author:
Affiliation:
1. Princeton University, Princeton, N J
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.2384
Reference9 articles.
1. Rhyming, I L and Yoler, Y A , "Supersonic boom of wingbody configurations, ' J Aerospace Sci 28, 313-320 (1961)
2. Morris, J , "An investigation of lifting effects on the intensity of sonic booms, ' J Roy Aeronaut Soc 64, 610-616 (1960)
3. The Shock Pattern of a Wing-Body Combination, Far from the Flight Path
4. September 1956;Whitham G B
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