Unsteady local linearization solution for pitching bodies of revolution at freestream Mach numbers = 1 - Stability derivative analysis
Author:
Affiliation:
1. Nielsen Engineering & Research, Inc., Mountain View, Calif.
2. Stanford University, Stanford, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference11 articles.
1. On the calculation of static and dynamic stability derivatives for bodies of revolution at subsonic and transonic speeds
Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Nonlinear unsteady supersonic flow analysis for slender bodies of revolution: Series solutions, convergence and results;Mathematical Problems in Engineering;1998
2. Nonlinear unsteady supersonic flow analysis for slender bodies of revolution: Theory;Mathematical Problems in Engineering;1997
3. Ad hoc closed form solutions of the two-dimensional non-linear steady small perturbation equation in fluid mechanics;International Journal of Non-Linear Mechanics;1995-07
4. Perturbation Solutions of Unsteady Transonic Flow over Bodies of Revolution;AIAA Journal;1978-12
5. Unsteady linearized transonic flow analysis for slender bodies;AIAA Journal;1977-07
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