Nozzle contours for minimum particle-lag loss
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/10.2514/3.2174
Reference5 articles.
1. Velocity Lag of Particles in Linearly Accelerated Combustion Gases
2. Recent Advances in Gas-Particle Nozzle Flows
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