Computational analysis of the flowfield of a two-dimensional ejectornozzle

Author:

CHOI Y.1,SOH W.1

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH; Sverdrup Technology, Inc., Brook Park, OH

Publisher

American Institute of Aeronautics and Astronautics

Reference22 articles.

1. Forced mixer lobes in ejector designs

2. University of Michigan Press,Ann Arbor, 1949,pp. 461-4623, 6.Porter, J.L.;Squyers,R.A.;and Nagaraja, K.S.: An Overview of Ejector 7. Deese, J.E.;and Agarwal, R.K.H.: A Numerical Study of Viscous Flow in

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1. Basic Study of the Ejector Effect, Part 2: Experimental Approach;47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2011-07-31

2. Basic Study of the Ejector Effect, Part 1: CFD;47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2011-07-31

3. Numerical Investigation of Inlet Induced Distortions of a Turbofan Engine Within an Indoor Test Facility;45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2009-08-02

4. Experimental Investigations on Macro-Aerodynamics Within a Jet Engine Ground Test Facility;45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2009-08-02

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