Department of Aerospace Engineering, Military Technical College, Cairo, Egypt.
10.21608/iugrc.2017.90952
Abstract
The dependence of aerodynamic features of a conventional missile on its configuration is examined. The features in concern are the zero-lift drag coefficient, the lift-curve slope and the center of pressure location. These coefficients are estimated using a home-made reliable tool that is used for conceptual design and preliminary sizing of rockets of simple shapes.
Abdel-Fattah, M., Hassan, A., & Ahmed, M. (2017). Preliminary Investigation on the Impact of Missile Design on its Aerodynamic Features. The International Undergraduate Research Conference, 2(Second International Undergraduate Research Conference, IUGRC), 65-65. doi: 10.21608/iugrc.2017.90952
MLA
Mahmoud M. Abdel-Fattah; Ahmed E. Hassan; Mahmoud Y. M. Ahmed. "Preliminary Investigation on the Impact of Missile Design on its Aerodynamic Features". The International Undergraduate Research Conference, 2, Second International Undergraduate Research Conference, IUGRC, 2017, 65-65. doi: 10.21608/iugrc.2017.90952
HARVARD
Abdel-Fattah, M., Hassan, A., Ahmed, M. (2017). 'Preliminary Investigation on the Impact of Missile Design on its Aerodynamic Features', The International Undergraduate Research Conference, 2(Second International Undergraduate Research Conference, IUGRC), pp. 65-65. doi: 10.21608/iugrc.2017.90952
VANCOUVER
Abdel-Fattah, M., Hassan, A., Ahmed, M. Preliminary Investigation on the Impact of Missile Design on its Aerodynamic Features. The International Undergraduate Research Conference, 2017; 2(Second International Undergraduate Research Conference, IUGRC): 65-65. doi: 10.21608/iugrc.2017.90952
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