Measurements of a simulated rocket exhaust plume near the Prandtl-Meyer limiting angle
- 1 April 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 12 (4) , 205-208
- https://doi.org/10.2514/3.27831
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Effect of nozzle boundary layers on rocket exhaust plumes.AIAA Journal, 1972
- Far field approximation for a nozzle exhausting into a vacuum.Journal of Spacecraft and Rockets, 1969
- A detonation tube technique for simulating rocket plumes in a space environment.Journal of Spacecraft and Rockets, 1968
- Exhaust plumes from nozzles with wall boundary layers.Journal of Spacecraft and Rockets, 1968
- Analytical approximation for the flow from a nozzle into a vacuum.Journal of Spacecraft and Rockets, 1966
- Untersuchung der thermischen Relaxation bei Düsenströmungen durch Analyse der gaskinetischen GeschwindigkeitsverteilungZeitschrift für Naturforschung A, 1960