Methods for determining the performance of ejector-diffuser systems.
Authors:
- 1 February 1966
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 3 (2) , 193-200
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- COMPARISON OF DIFFUSER-EJECTOR PERFORMANCE WITH FIVE DIFFERENT DRIVING FLUIDS1963
- SHOCK-INDUCED BOUNDARY LAYER SEPARATION IN OVER-EXPANDED CONICAL EXHAUST NOZZLESAIAA Journal, 1963
- High Altitude and Space Simulation TestingARS Journal, 1962
- THE EFFECT OF SECOND THROAT GEOMETRY ON THE PERFORMANCE OF EJECTORS WITHOUT INDUCED FLOW1961
- EFFECTS OF DIFFUSER LENGTH ON THE PERFORMANCE OF EJECTORS WITHOUT INDUCED FLOW1961
- SOME REYNOLDS NUMBER EFFECTS ON THE PERFORMANCE OF EJECTORS WITHOUT INDUCED FLOW1961