A Numerical Study Into a Local Protuberance Interaction With a Fin On A Supersonic Projectile
Author:
Affiliation:
1. The Queen's University of Belfast
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-1092
Reference8 articles.
1. 1Massey, K. C., McMichael, J., Warnock. T., and Hay, F. "Mechanical Actuators for Guidance of a Supersonic Projectile," AIAA Paper2005-4970,2005
2. A Survey of the Effects of Small Protuberances on Boundary-Layer Flows
3. Step induced boundary-layer separation phenomena
4. Survey of viscous interactions associated with high Mach number flight
5. 5Dillenius, D., and Lesieutre, D. "Prediction of the Nonlinear Aerodynamic Characteristics of Tandem Controland RollingTail Missiles," AIAA Paper 2002-4511,2002
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