Mathematical phenomenology for thrust-vectoring-induced agility comparisons-Reference-Cited by-同舟云学术

Mathematical phenomenology for thrust-vectoring-induced agility comparisons

Published:1993-03 Issue:2 Volume:30 Page:248-255
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Gal-Or Benjamin¹,Baumann Daniel D.²

Affiliation:

1. Technion — Israel Institute of Technology, Haifa 32000, Israel

2. Flight Dynamics Directorate, Wright-Patterson Air Force Base, Ohio

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.48273

Reference21 articles.

1. Fundamental concepts of vectored propulsion

2. Agile Fighter Aircraft Simulation

3. 5Baumann, D. D. "F-15B High-Angle-of-Attack Phenomena and Spin Prediction Using Bifurcation Analysis," M.S. Thesis, Aeronautical Engineering,Air ForceInst. of Technology, AFIT/GAE/ENY/ 89D-01, Wright-Patterson AFB, OH,Dec. 1989; see also Planeaux, J. B., and Baumann, D. D. "Bifurcation Analysis of a Model Fighter Aircraft with Control Augmentation,"AIAA Paper90-2836, 1990.

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