Boundary-layer turbulence measurements with mass addition and combustion.
Author:
Affiliation:
1. United Technology Center, Sunnyvale, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.3832
Reference34 articles.
1. TURBULENT BOUNDARY LAYER COMBUSTION IN THE HYBRID ROCKET
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