The experimental data were aimed at obtaining the effect of jet mixing, the effective length/diameter of the ejector tube, the entrance length shape factor, the shape loading, and the optimum primary jet location. The total augmented thrust is proportional to the diameter of the ejector. The data show that for a practical design the entrance lip shape and the stream lines around the lip are also important in order to optimize the percentage augmentation.
Experimental study on optimization parameters of a supersonic jet ejector thrust augmentor.
Journal of Aircraft ; 10
1973-09-01
Miscellaneous
No indication
English
FULL-LENGTH PAPERS - Pulsed-Jet Ejector Thrust Augmentor Characteristics
Online Contents | 2012
|Thrust augmentor inlet optimization
AIAA | 1986
|NTIS | 1971
|