Wind-tunnel measurement at M equal 4.28 of some static and dynamic aerodynamic characteristics of finned missiles suspended magnetically.
- 1 July 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 5 (7) , 838-842
- https://doi.org/10.2514/3.29367
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Measured aerodynamic characteristics of a cone- cylinder-cone model with base separation at M equal 4.8.Journal of Spacecraft and Rockets, 1965
- Studies of wakes of support-free spheres at m equal 16 in heliumAIAA Journal, 1965
- ROLL DAMPING MOMENT MEASUREMENTS FOR THE BASIC FINNER AT SUBSONIC AND SUPERSONIC SPEEDSPublished by Defense Technical Information Center (DTIC) ,1964
- Magnetic Suspension and Balance System for Wind Tunnel ApplicationJournal of the Royal Aeronautical Society, 1963