1 |
Harvey, J. K., "Some Measurements on a Yawed Slender Delta Wing with Leading Edge Separation," ARC R & M 3160, 1961.
|
2 |
Wood, N. J., Robert, L., and Cellik, Z., "Control of Asymmetric Vortical Flows over Delta Wings at High Angles of Attack," J. of Aircraft, Vol. 27, No. 5, 1990, pp. 429-435.
DOI
|
3 |
이기영, 손명환, 장영일, "Investigation of Vortex Interactions over a Delta Wing with the Leading Edge Extension," 한국군사기술학회 종합학술대회, August 2001.
|
4 |
Verhaagen, N. G., and Naarding, S. H. J., "Experimental and Numerical Investigation of the Vortex Flow over a Yawed Delta Wing," AIAA Paper 88-2563, June 1988.
|
5 |
Herbbar, S. K., Platzer, M. F., and Chang, W-H, "Control of High-Incidence Vortical Flow on Double-Delta Wings Undergoing Sideslip," J. of Aircraft, Vol. 34, No. 4, 1997, pp. 506-513.
DOI
ScienceOn
|
6 |
Schrader, K. F., Reynolds, G. A., and Novak, C. J., "Effects of Mach Number and Reynolds Number on Leading-Edge Vortices at High Angle-of-Attack," AIAA paper 88-0122, January 1988.
|
7 |
Ericsson, L. E., "Vortex Characteristics of Pitching Double-Delta Wings," J. of Aircraft, Vol. 36, No. 2, 1999, pp. 349-356.
DOI
ScienceOn
|
8 |
Grismer, D. S., "Double-Delta-Wing Aerodynamics for Pitching Motions with and without Sideslip," J. of Aircraft, Vol. 32, No. 6, 1995, pp. 1303-1311.
DOI
|
9 |
손명환, 이기영, "Vortex Flow Control in Modern Aerodynamics," 한국항공우주학회지 제28권 7호, 2000.,10., pp. 119-130.
|
10 |
손명환, 이기영, 백승욱, "Effects of Sideslip on the Vortex Flow over a Delta Wing with the Leading Edge Extension," 한국항공우주학회 춘계학술대회, April 2001.
|
11 |
Erickson, G. E., Schreiner, J. A., & Rogers, L. W., "On the Structure, Interaction, and Breakdown Characteristics of Slender Wing Vortices at Subsonic, Transonic, and Supersonic Speeds," AIAA paper 89-3345. August 1989.
|
12 |
Bannink, W. J., Some Recent Results on Vortex Bursting on a Delta Wing at High Subsonic Speeds, AGARD-CP-437, Vol. 1, 1988.
|
13 |
Malcolm, G. N., "Impact of High-Alpha Aerodynamics on Dynamic Stability Parameters of Aircraft and Missiles, "AGARD-CS-114, paper No. 2, 1981.
|