References
- Wardlaw, A. B., Morrison, A. M., "Induced Side Forces at High Angles of Attack", J. Spacecraft, Vol. 13, No. 10, pp. 589-593, 1976. https://doi.org/10.2514/3.27931
- Keener, E. R., Chapman, G. T., Cohen, L. and Talaghani, J., "Side Forces on a Tangent-Ogive Forebody with a Fineness Ratio of 3.5 at High Angles of Attack and Mach Numbers from 0.1 to 0.7", NASA TM X-3437, 1977.
- Deng, X. Y., Tian, W., Ma, B. F. and Wang, Y. K., "Recent Progress on the Study of Asymmetric Vortex Flow over Slender Bodies", Acta Mech Sin, Vol. 24, pp. 475-487, 2008. https://doi.org/10.1007/s10409-008-0197-3
- Williams, D., "A Review of Fore Body Vortex Control Scenarios", AIAA paper 97-1967, 1997.
- Bernhardt, J. E. and Williams, D. R., "Proportional Control of Asymmetric Forebody Vortices", AIAA Journal, Vol. 36, No. 11, pp. 2087-2093, 1998. https://doi.org/10.2514/2.310
- Matsuno, T., Kawazoe, H., Nelson, R. C., T. C., Corke, "Forebody Vortex Control on High Performance Aircraft Using PWM-Controlled Plasma Actuators", 26th International Congress of the Aeronautical Sciences, 2008.
- Poon, D., Simon, T., Kortshagen, U. and Ernie, D., "Experimental Studies of Plasma Actuator Performance for Separation Control", AIAA paper 2010-1219, 2010.
- E. S. Lee, J. I. Lee, and K. S. Lee, "Numerical Investigation of the Behavior of the Blowing Actuator for Body Vortex Control", KSCFE Conference, Nov. 2011.
-
Park, S. H. and Kwon, J. H., "Implementation of k-
$\omega$ Turbulence Models in an Implicit Multigrid Method", AIAA Journal, Vol. 42, No. 7, pp. 1348-1357, 2004. https://doi.org/10.2514/1.2461