Boundary-layer transition and dynamic sting interference
- 1 October 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (10) , 1886-1888
- https://doi.org/10.2514/3.6012
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- On the calculation of static and dynamic stability derivatives for bodies of revolution at subsonic and transonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- Effect of boundary-layer transition on vehicle dynamicsJournal of Spacecraft and Rockets, 1969
- Some Integrals Relating to the Vibration of a Cantilever Beam and Approximation for the Effect of Taper on Overtone FrequenciesAeronautical Quarterly, 1956