Bifurcation analysis of aircraft pitching motions about large mean angles of attack
- 1 January 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 7 (1) , 113-122
- https://doi.org/10.2514/3.8553
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Nonlinear aerodynamic modeling of flap oscillations in transonic flow - A numerical validationAIAA Journal, 1983
- Unsteady Newton-Busemann flow theory. I - AirfoilsAIAA Journal, 1981
- Elementary Stability and Bifurcation TheoryPublished by Springer Nature ,1980
- Large-amplitude slow oscillation of wedges in inviscid hypersonic and supersonic flowsAIAA Journal, 1970
- Stability of oscillating wedges and caret wings in hypersonic and supersonic flows.AIAA Journal, 1969