Particle injection into a uniform flow
Author:
Affiliation:
1. The Johns Hopkins University, Applied Physics Laboratory, Silver Spring, Md.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.30061
Reference4 articles.
1. Drag coefficient of particles in a rocket nozzle.
2. An experimental and comparative study of jet penetration in supersonic flow.
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Particle injection into an incompressible laminar boundary layer flow along a semi-infinite flat plate;1st National Fluid Dynamics Conference;1988-07-25
2. Bases for predicting gas-particle flows with particular reference to turbomachinery;International Journal of Heat and Fluid Flow;1983-06
3. Penetration of Particles Injected into a Constant Cross Flow;AIAA Journal;1974-08
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