000 015280000a22003250004500
003 EG-GiCUC
005 20250223025716.0
008 081228s2008 ua dh f m 000 0 eng d
040 _aEG-GiCUC
_beng
_cEG-GiCUC
041 0 _aEng
049 _aDeposite
097 _aM.Sc
099 _aCai01.13.01.M.Sc.2008.Mo.V
100 0 _aMohamed Hassan Ali
245 1 0 _aVariable fidelity design optimization of subsonic aircraft air intake /
_cMohamed Hassan Ali ; Supervised Mohamed Madbouli Abdelrahman
246 1 5 _aدراسة متعددة الثقة للحصول على أفضل تصميم لمدخل الهواء للطائرات
260 _aCairo :
_bMohamed Hassan Ali ,
_c2008
300 _a113P. :
_bcharts , facsimiles ;
_c30cm
502 _aThesis(M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
520 _aThe 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
530 _aIssued also as CD
653 4 _aFinite element
653 4 _aFlutter
653 4 _aPiezoelectric
700 0 _aMohamed Madbouli Abdelrahman ,
_eSupervisor
856 _uhttp://172.23.153.220/th.pdf
905 _aMustafa
_eRevisor
905 _aSamia
_eCataloger
942 _2ddc
_cTH
999 _c18920
_d18920