An Analysis of Asymmetric Rolling Bodies with Nonlinear Aerodynamics
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Va.
2. Sandia Laboratories, Albuquerque, N. Mex.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference10 articles.
1. Nonlinear motion of a missile with slight configurational asymmetries
2. Resonance instability for finned configurations having nonlinear aerodynamic properties
3. Perturbation Methods
4. Response of an Asymmetric Missile to Spin Varying through Resonance
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