Bifurcation analysis in the flight dynamics design process? A view from the aircraft industry-Reference-Cited by-同舟云学术

Bifurcation analysis in the flight dynamics design process? A view from the aircraft industry

Published:1998-10-15 Issue:1745 Volume:356 Page:2321-2333
ISSN:1364-503X
Container-title:Philosophical Transactions of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences
language:en
Short-container-title:Philosophical Transactions of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences

Author:

Macmillen F. B. J.¹,Thompson J. M. T.²

Affiliation:

1. Flight Sciences Department, Bombardier Aerospace Inc.,400 Chemin de la Côte Vertu, Montreal, Quebec, Canada H4S 1Y9

2. Department of Mathematics, University College London, Gower Street, London WC1E 6BT, UK

Publisher

The Royal Society

Subject

General Physics and Astronomy,General Engineering,General Mathematics

Link

Reference32 articles.

3. Baumann D. D. 1989 F-15B high angle-of-attack phenomena and spin prediction using bifurcation analysis. MSc thesis AFIT/GAE/ENY/89D-01 891200.

5. Davison M. T. 1992 An examination of wing rock for the F-15. MSc thesis AFIT/GAE/ ENY/92m-01 9202000.

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