Three-dimensional flow in rotating rocket motor nozzles
- 1 March 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 23 (2) , 207-214
- https://doi.org/10.2514/3.25101
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Flowfield Computations in Rotating Propulsive NozzlesAIAA Journal, 1980
- Transonic Potential Flow around Axisymmetric Inlets and Bodies at Angle of AttackAIAA Journal, 1977
- Gas Dynamic Gain of Supersonic Thrust NozzlesJournal of Spacecraft and Rockets, 1974
- Transonic flow in small throat radius of curvature nozzles.AIAA Journal, 1969