Affiliation:
1. DLR, German Aerospace Research Center, D-74239 Lampoldshausen, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Reference23 articles.
1. Experimental study of boundary layer separation in truncated ideal contour nozzles
2. LawrenceR. A. “Symmetrical and Unsymmetrical Flow Separation in Supersonic Nozzles,” NASA CR 92587, Ph.D. Thesis, Institute of Technology of Southern Methodist University, Dallas, TX, April 1967.
3. Restricted Shock Separation in Rocket Nozzles
4. Sea level side loads in high-area-ratio rocket engines
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