Preliminary Investigation on the Impact of Missile Design on its Aerodynamic Features | ||
| The International Undergraduate Research Conference | ||
| Article 73, Volume 2, Second International Undergraduate Research Conference, IUGRC, 2017, Pages 65-65 PDF (492.51 K) | ||
| Document Type: Original Article | ||
| DOI: 10.21608/iugrc.2017.90952 | ||
| Authors | ||
| Mahmoud M. Abdel-Fattah; Ahmed E. Hassan; Mahmoud Y. M. Ahmed | ||
| Department of Aerospace Engineering, Military Technical College, Cairo, Egypt. | ||
| 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. | ||
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