Theory of Steady Flow with Mass Addition Applied to Solid Propellant Rocket Motors
- 1 July 1953
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the American Rocket Society
- Vol. 23 (4) , 237-241
- https://doi.org/10.2514/8.4600
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Steady-State One-Dimensional Flow in Rocket MotorsJournal of Applied Physics, 1952
- On the Steady Flow of a Gas Through a Tube with Heat Exchange or Chemical ReactionJournal of the Aeronautical Sciences, 1946
- Characteristics of the rocket motor unit based on the theory of perfect gasesJournal of the Franklin Institute, 1940