Forward Flight Effects on Counterflow Thrust Vector Control of a Supersonic Jet-Reference-Cited by-同舟云学术

Forward Flight Effects on Counterflow Thrust Vector Control of a Supersonic Jet

Published:1999-02 Issue:2 Volume:37 Page:279-281
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Alvi F. S.¹,Strykowski P. J.²

Affiliation:

1. Florida A&M University and Florida State University, Tallahassee, Florida 32310

2. University of Minnesota, Minneapolis, Minnesota 55455

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.705

Reference5 articles.

1. Multi-axis fluidic thrust vectoring of supersonic jets via counterflow

2. Multiaxis fluidic thrust vector control of a supersonic jet using counterflow

3. Counterflow thrust vectoring of supersonic jets

4. 5Wishart, D. P. “The Structure of a Heated Supersonic Jet Operating at Design and Off-Design Conditions,”Ph.D. Dissertation,Dept. of Mechanical Engineering, Florida StateUniv., Tallahassee, FL,April 1995.

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