Exhaust Nozzle Contour for Optimum Thrust
Author:
Affiliation:
1. Marquardt Aircraft Co., Van Nuys, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.7324
Reference5 articles.
1. The Analytical Design of an Axially Symmetric Laval Nozzle for a Parallel and Uniform Jet
2. A Philosophy for Improved Rocket Nozzle Design
3. Shapiro, A. H. "The Dynamics and Thermodynamics of Compressible Fluid Flow," Ronald Press, New York, pp.676-680.
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