Please use this identifier to cite or link to this item:
|Title:||Aerodynamic assessment of the baseline configuration of a rocket : theoretical and numerical||Authors:||Omar, Zaki Al||Advisors:||Jadayel, Oussama Chafiq||Subjects:||Rockets (Aeronautics)||Issue Date:||2018||Description:||
Includes bibliographical references (p. 79-82).
Supervised by Dr. Oussama Jadayel.
|URI:||https://scholarhub.balamand.edu.lb/handle/uob/4140||Rights:||This object is protected by copyright, and is made available here for research and educational purposes. Permission to reuse, publish, or reproduce the object beyond the personal and educational use exceptions must be obtained from the copyright holder||Type:||Thesis|
|Appears in Collections:||UOB Theses and Projects|
Show full item record
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.