A Philosophy for Improved Rocket Nozzle Design
- 1 October 1957
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Jet Propulsion
- Vol. 27 (10) , 1088-1093
- https://doi.org/10.2514/8.12463
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- A Mechanism for High-Frequency Oscillation in Ramjet Combustors and AfterburnersJournal of Jet Propulsion, 1956
- Combustion instability in solid-propellant rocketsSymposium (International) on Combustion, 1953
- Experimental investigation of combustion instability in rocket motorsSymposium (International) on Combustion, 1953
- Combustion Studies with a Rocket Motor Having a Full-Length Observation WindowJournal of the American Rocket Society, 1952
- Shatter of Drops in Streams of AirIndustrial & Engineering Chemistry, 1951