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200 00$aNorthrop F-5 case study in aircraft design$b[electronic resource] /$fpresented by William G. Stuart
210   $a[Hawthorne, Calif. $cNorthrop Corp.$d1978]
215   $a1 online resource (220 p.)
225 1 $aAIAA professional study series
300   $aCover title.
311   $a1-56347-309-7 
327   $a""COVER ""; ""ABSTRACT""; ""INTRODUCTION""; ""1950's CHANGINGS ENVIRONMENT""; ""AERODYNAMICS""; ""COMBAT PERFORMANCE PARAMETERS""; ""INTUITION Vs REALITY""; ""MAINTENANCE""; ""DESIGN LESSONS""; ""STRESS CORROSION INHIGH STRENGTH ALUMINUM ALLOYS""; ""SPECIFIC SYSTEM DESIGN PROBLEMS""; ""PILOT INDUCED OSCILLATIONS (PIO) T-38/F-5""; ""SURVIVABILITY""; ""AVIONICS DEVELOPMENT""; ""AVIONICS SYSTEM REQUIREMENTS""; ""AVIONIC8 SYSTEMS IMPLEMENTATION TASKS""; ""SUMMARY""
410  0$aAIAA professional study series.
606   $aJet planes, Military
606   $aAirplanes, Military
615  0$aJet planes, Military.
615  0$aAirplanes, Military.
676   $a623.7/465
701   $aStuart$b William G$01514954
712 02$aNorthrop Corp.$bAircraft group.
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