Aircraft Mechanics Department, Military Technical College, Cairo, Egypt.
10.21608/iugrc.2017.90916
Abstract
Motivated by the design of a MALE UAV for a military mission. The aerodynamic characteristics for the basic geometry of a UAV (MALE configuration) are calculated using USAF Digital DATCOM. Also, we calculated the aerodynamic characteristics of the UAV with deflected control surface for the same configuration. Furthermore, we estimate the stability and control derivative based on the required mission specification and flight envelope for the suggested design.
Ibrahim, N. E., Zakaria, M., & Elsebaie, A. (2017). Calculating Aerodynamic & Stability Characteristics for a MALE UAV using USAF Digital DATCOM. The International Undergraduate Research Conference, 2(Second International Undergraduate Research Conference, IUGRC), 63-63. doi: 10.21608/iugrc.2017.90916
MLA
Nour ELdein Ahmed Ibrahim; Mohamed Y. Zakaria; Ahmed Mohamed Elsebaie. "Calculating Aerodynamic & Stability Characteristics for a MALE UAV using USAF Digital DATCOM". The International Undergraduate Research Conference, 2, Second International Undergraduate Research Conference, IUGRC, 2017, 63-63. doi: 10.21608/iugrc.2017.90916
HARVARD
Ibrahim, N. E., Zakaria, M., Elsebaie, A. (2017). 'Calculating Aerodynamic & Stability Characteristics for a MALE UAV using USAF Digital DATCOM', The International Undergraduate Research Conference, 2(Second International Undergraduate Research Conference, IUGRC), pp. 63-63. doi: 10.21608/iugrc.2017.90916
VANCOUVER
Ibrahim, N. E., Zakaria, M., Elsebaie, A. Calculating Aerodynamic & Stability Characteristics for a MALE UAV using USAF Digital DATCOM. The International Undergraduate Research Conference, 2017; 2(Second International Undergraduate Research Conference, IUGRC): 63-63. doi: 10.21608/iugrc.2017.90916
)
View on SCiNiTO