One-Dimensional, Steady Flow with Mass Addition and the Effect of Combustion Chamber Flow on Rocket Thrust with a Supplement on the Integration of the Burning Equation
- 1 February 1955
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Jet Propulsion
- Vol. 25 (2), 61-66
- https://doi.org/10.2514/8.6598
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Erosive Burning of Some Composite Solid PropellantsJournal of Jet Propulsion, 1954
- Theory of Steady Flow with Mass Addition Applied to Solid Propellant Rocket MotorsJournal of the American Rocket Society, 1953
- Steady-State One-Dimensional Flow in Rocket MotorsJournal of Applied Physics, 1952
- Note on straight pipe jet motorsCommunications on Pure and Applied Mathematics, 1949
- The Mechanics and Thermodynamics of Steady One-Dimensional Gas FlowJournal of Applied Mechanics, 1947