Nonlinear motion of a symmetric missile acted on by a double valued static moment.
- 1 April 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (4) , 713-717
- https://doi.org/10.2514/3.4568
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Slender body estimates for two cubic aerodynamic damping moments.AIAA Journal, 1966
- Angular motion of a re-entering symmetric missileAIAA Journal, 1965
- Quasi-linear analysis of the nonlinear motion of a nonspinning symmetric missileZeitschrift für angewandte Mathematik und Physik, 1963
- Circular pitching and yawing motion of nose cone configurationsPlanetary and Space Science, 1961
- The Prediction of Nonlinear Pitching and Yawing Motion of Symmetric MissilesJournal of the Aeronautical Sciences, 1957