Approximate far-field flow description for a nozzle exhausting into a vacuum
- 1 November 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 7 (11) , 1374-1376
- https://doi.org/10.2514/3.30177
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- COMBUSTION RESIDUES FROM N2O4-MMH MOTORSPublished by Defense Technical Information Center (DTIC) ,1969
- Preignition Products from Propellants at Simulated High-Altitude ConditionsCombustion Science and Technology, 1969
- Far field approximation for a nozzle exhausting into a vacuum.Journal of Spacecraft and Rockets, 1969
- Analytical approximation for the flow from a nozzle into a vacuum.Journal of Spacecraft and Rockets, 1966
- Approximate computation of underexpanded jet structureAIAA Journal, 1965