Experimental Study of an Axisymmetric Dual Throat Fluidic Thrust Vectoring Nozzle for Supersonic Aircraft Application-Reference-Cited by-同舟云学术

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Experimental Study of an Axisymmetric Dual Throat Fluidic Thrust Vectoring Nozzle for Supersonic Aircraft Application

Published:2007-07-08 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Flamm Jeffrey,Deere Karen,Mason Mary,Berrier Bobby,Johnson Stuart

Publisher

American Institute of Aeronautics and Astronautics

Reference12 articles.

1. 3Waithe, Kenrick A.: An Experimental and Computational Investigation of Multiple Injection Ports in a Convergent-Divergent Nozzle for FluidicThrustVectoring. Master of ScienceThesis, May 2001.

2. 4Deere, K.A.: Computational Investigation of theAerodynamic Effects on FluidicThrustVectoring. AIAA2000-3598, July 2000.

3. Computational investigation of circular-to-rectangular transition ducts

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