Single Expansion Ramp Nozzles: Impact of Ramp Length on Flow and Acoustics
Author:
Affiliation:
1. University of Cincinnati, Cincinnati, OH 45221
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J059386
Reference25 articles.
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3. EngblomW. A. “Numerical Prediction of SERN Performance Using WIND Code,” AIAA Paper 2003-4410, 2003.
4. LanderJ.PalczaJ. “Exhaust Nozzle Deflector Systems for V/STOL Fighter Aircraft,” AIAA Paper 1974-1169, 1974.
5. DusaD. J.SpeirD. W.RoweR. K. “Advanced Technology Exhaust Nozzle Development,” AIAA Paper 1983-1286, 1983.
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