Effect of Spike Truncation on the Acoustic Behavior of Annular Aerospike Nozzles
Author:
Affiliation:
1. Experimental Aerodynamics Division, National Aerospace Laboratories, Bangalore 560 017, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052139
Reference52 articles.
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5. Lift-Off Acoustics Predictions for the Ares I Launch Pad
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