Multi-Directional Co-Flow Fluidic Thrust Vectoring Intended for a Small Gas Turbine-Reference-Cited by-同舟云学术

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Multi-Directional Co-Flow Fluidic Thrust Vectoring Intended for a Small Gas Turbine

Published:2007-05-07 Issue: Volume: Page:
ISSN:
Container-title:AIAA Infotech@Aerospace 2007 Conference and Exhibit
language:
Short-container-title:

Author:

Banazadeh Afshin¹,Saghafi Fariborz¹,Ghoreyshi Mehdi²,Pilidis Pericles²

Affiliation:

1. Sharif University of Technology

2. Cranfield University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-2940

Reference23 articles.

1. R. Lewis, "Optimization of a thrust vectoring system for the next generation fighter aircraft", M.Sc. Thesis,Cranfield University, 2004

2. A review of thrust-vectoring schemes for fighter applications

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