Results from a new wind-tunnel apparatus for studying coning and spinning motions of bodies of revolution
- 1 November 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (11) , 1953-1957
- https://doi.org/10.2514/3.6031
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Aerodynamics of bodies of revolution in coning motion.AIAA Journal, 1969
- Effect of boundary-layer transition on dynamic stability.Journal of Spacecraft and Rockets, 1966
- FREE FLIGHT MOTION OF SYMMETRIC MISSILESPublished by Defense Technical Information Center (DTIC) ,1963
- Laminar Boundary Layer on a Spinning Cone at Small Angles of Attack in a Supersonic FlowJournal of the Aeronautical Sciences, 1957