Exhaust Nozzle Contour for Optimum Thrust
- 1 June 1958
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Jet Propulsion
- Vol. 28 (6), 377-382
- https://doi.org/10.2514/8.7324
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- A Philosophy for Improved Rocket Nozzle DesignJournal of Jet Propulsion, 1957
- The Analytical Design of an Axially Symmetric Laval Nozzle for a Parallel and Uniform JetJournal of the Aeronautical Sciences, 1949