02114nam 2200565 a 450 991045721670332120200520144314.01-60086-869-X1-60086-830-4(CKB)2550000000073499(EBL)3111490(SSID)ssj0000646967(PQKBManifestationID)12283049(PQKBTitleCode)TC0000646967(PQKBWorkID)10592292(PQKB)11593757(MiAaPQ)EBC3111490(Au-PeEL)EBL3111490(CaPaEBR)ebr10516586(OCoLC)922978711(EXLCZ)99255000000007349919800102d1978 uy 0engur|n|---|||||txtccrNorthrop F-5 case study in aircraft design[electronic resource] /presented by William G. Stuart[Hawthorne, Calif. Northrop Corp.1978]1 online resource (220 p.)AIAA professional study seriesCover title.1-56347-309-7 ""COVER ""; ""ABSTRACT""; ""INTRODUCTION""; ""1950's CHANGINGS ENVIRONMENT""; ""AERODYNAMICS""; ""COMBAT PERFORMANCE PARAMETERS""; ""INTUITION Vs REALITY""; ""MAINTENANCE""; ""DESIGN LESSONS""; ""STRESS CORROSION INHIGH STRENGTH ALUMINUM ALLOYS""; ""SPECIFIC SYSTEM DESIGN PROBLEMS""; ""PILOT INDUCED OSCILLATIONS (PIO) T-38/F-5""; ""SURVIVABILITY""; ""AVIONICS DEVELOPMENT""; ""AVIONICS SYSTEM REQUIREMENTS""; ""AVIONIC8 SYSTEMS IMPLEMENTATION TASKS""; ""SUMMARY""AIAA professional study series.Jet planes, MilitaryAirplanes, MilitaryElectronic books.Jet planes, Military.Airplanes, Military.623.7/465Stuart William G954724Northrop Corp.Aircraft group.MiAaPQMiAaPQMiAaPQBOOK9910457216703321Northrop F-5 case study in aircraft design2159449UNINA