TY  - GEN
AU  - Mohamed Hassan Ali
AU  - Mohamed Madbouli Abdelrahman , 
TI  - Variable fidelity design optimization of subsonic aircraft air intake / 
PY  - 2008///
CY  - Cairo : 
PB  - Mohamed Hassan Ali , 
KW  - Finite element
KW  - Flutter
KW  - Piezoelectric
N1  - Thesis(M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering; Issued also as CD
N2  - The aircraft air intake is one of the most important parts in the layout design of modern fighter and trainer aircraft most of the aircrafts famous for their good maneuvers have a well designed air intake which is capable of tolerating high angles of attack and large sideslip angles without significant pressure losses and the engine thrust in return
UR  - http://172.23.153.220/th.pdf
ER  -