Steady-State Circular Pitching and Yawing Motion of Symmetric Missiles
- 1 September 1959
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 26 (9) , 600-601
- https://doi.org/10.2514/8.8212
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- The Prediction of Nonlinear Pitching and Yawing Motion of Symmetric MissilesJournal of the Aeronautical Sciences, 1957
- PREDICTION OF THE MOTION OF MISSILES ACTED ON BY NON-LINEAR FORCES AND MOMENTSPublished by Defense Technical Information Center (DTIC) ,1956
- The Estimation of Normal-Force, Drag, and Pitching-Moment Coefficients for Blunt-Based Bodies of Revolution at Large Angles of AttackJournal of the Aeronautical Sciences, 1954
- Aerodynamic symmetry of projectilesQuarterly of Applied Mathematics, 1949