Design of Maximum Thrust Plug Nozzles for Fixed Inlet Geometry
Author:
Affiliation:
1. U.S. Air Force Academy, Colo.
2. Purdue University, Lafayette, Ind.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49960
Reference12 articles.
1. Exhaust Nozzle Contour for Optimum Thrust
2. Spike nozzle contour for optimum thrust
3. Optimum thrust-nozzle contours for gas-particle flows.
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