Wind Tunnel Test of an Unmanned Aerial Vehicle (UAV) |
Chung, Jin-Deog
(Korea Aerospace Research Institute, Senior Engineering)
Lee, Jang-Yeon (Korea Aerospace Research Institute, Principle Engineering) Sung, Bong-Zoo (Korea Aerospace Research Institute, Principle Engineering) Koo, Sa-Mok (Korea Aerospace Research Institute, Principle Engineering) |
1 | Helwani, M., Shockey, G. A., Smith, R. L., Thompson, T. L., 2001, 'Wind Tunnel Test Results for a Canard Rotor/Wing Aircraft Configuration,' 57th American Helicopter Society Meeting May 9-11 |
2 | Arnette, S. A., Porter, C. B., Meredith, W. S., Hoffman, J. M. and Sung, B. Z., 2000, 'Aerodynamic Commissioning Results for the Korea Aerospace Research Institute Low Speed Wind Tunnel,' AIAA-2000-0291, 38TH Aerospace Sciences Meeting & Exhibit, Reno, NV |
3 | Bass, S. M., Thompson, T. L., Rutherford, J. W., 1993, 'Canard Rotor/Wing : A revolutionary High-Speed Rotorcraft concept,' AIAA-93-1175, Aerospace Design Conference, Irvine, CA |
4 | Chung, J, Cho, T., Sung, B. and Lee, J, 'Wind Tunnel Test of a Canard Airplane,' KSME international Journal, Vol. 16, No.1, pp. 125-131 과학기술학회마을 |