Static investigation of a fixed-aperture nozzle employing fluidic injection for multiaxis thrust vector control-Reference-Cited by-同舟云学术

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Static investigation of a fixed-aperture nozzle employing fluidic injection for multiaxis thrust vector control

Published:1997-07-06 Issue: Volume: Page:
ISSN:
Container-title:33rd Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Giuliano Victor¹,Wing David²,Giuliano Victor¹,Wing David²

Affiliation:

1. Pratt & Whitney, West Palm Beach, FL

2. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-3149

Reference7 articles.

1. Thrust Vectoring of an Axisymmetric Exhaust Nozzle at Static Conditions. ASME FEDSM97-3228,June, 1997.

2. Characteristics of Thrust-Vectored Axisymmetric Ejector Nozzles. NASATM-4610,March, 1995.

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