Application of bifurcation theory to the high-angle-of-attack dynamics of the F-14-Reference-Cited by-同舟云学术

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Application of bifurcation theory to the high-angle-of-attack dynamics of the F-14

Published:1994-01 Issue:1 Volume:31 Page:26-34
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Jahnke C. C.¹,Culick F. E. C.²

Affiliation:

1. Clarkson University, Potsdam, New York 13699

2. California Institute of Technology, Pasadena, California 91125

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.46451

Reference20 articles.

1. Note on a Criterion for Severity of Roll-Induced Instability

2. Pseudosteady state analysis of nonlinear aircraft maneuvers

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