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, Page 65-65 PDF (492.51 K) | ||||
| Document Type: Original Article | ||||
| DOI: 10.21608/iugrc.2017.90952 | ||||
 View on SCiNiTO | ||||
| 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. | ||||
|
Statistics Article View: 41 PDF Download: 35 |
||||
