Aerodynamic Effects Induced by a Vectored High Aspect Ratio Nonaxisymmetric Exhaust Nozzle
Author:
Affiliation:
1. Air Force Flight Dynamics Laboratory, Wright-Palterson Air Force Base, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.58557
Reference7 articles.
1. Nonaxisymmetric Nozzles Installed in Advanced Fighter Aircraft
2. An investigation of induced drag reduction through over-the-wing blowing
3. Supercirculation Effects Induced by Vectoring a Partial-Span Rectangular Jet
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1. Elements of Aerodynamic Model Validation for Delta-Canard Configured Aircraft with Thrust-Vectoring;IFAC Proceedings Volumes;1997-07
2. Trailing-edge jet control of leading-edge vortices of a delta wing;AIAA Journal;1996-07
3. Swirling flows in circular-to-rectangular transition ducts;Experiments in Fluids;1996-04
4. Flow distortion in a circular-to-rectangular transition duct;AIAA Journal;1990-08
5. Experimental definition of nonaxisymmetric exhaust nozzle plumes;Journal of Aircraft;1985-03
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