On the Pure Rolling Motion of Winged And/Or Finned Missiles in Varying Supersonic Flight
- 1 March 1953
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 20 (3) , 160-168
- https://doi.org/10.2514/8.2580
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- A Method of Determining Some Aerodynamic Coefficients from Supersonic Free-Flight Tests of a Rolling MissileJournal of the Aeronautical Sciences, 1950
- Some Ballistic Contributions to AerodynamicsJournal of the Aeronautical Sciences, 1947
- The Aerodynamic Performance of Small Spheres from Subsonic to High Supersonic VelocitiesJournal of the Aeronautical Sciences, 1945