Effect of nozzle boundary layers on rocket exhaust plumes.
- 1 November 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (11) , 1534-1535
- https://doi.org/10.2514/3.6656
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Approximate far-field flow description for a nozzle exhausting into a vacuumJournal of Spacecraft and Rockets, 1970
- Far field approximation for a nozzle exhausting into a vacuum.Journal of Spacecraft and Rockets, 1969
- Exhaust plumes from nozzles with wall boundary layers.Journal of Spacecraft and Rockets, 1968
- Highly underexpanded jet structure - Exact and approximate calculations.AIAA Journal, 1967
- Analytical approximation for the flow from a nozzle into a vacuum.Journal of Spacecraft and Rockets, 1966
- Hypersonic boundary-layer separation and the base flow problem.AIAA Journal, 1966
- Rapid expansion of a supersonic boundary layer and its application to the near wake.AIAA Journal, 1966
- FAR-FIELD APPROXIMATION FOR A NOZZLE EXHAUSTING INTO A VACUUMAIAA Journal, 1963