Northrop F-5 case study in aircraft designThis case study describes the overall development of the T-38/F-5 family of fighter/trainer aircraft in terms of configuration development motivation and constraints. Selected systems are examined in detail, including the constraints, specifications, and trade-offs that led to important design decisions. |
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Häufige Begriffe und Wortgruppen
aerodynamic aileron air combat maneuvering airframe airplane alloys altitude angle of attack area ruling arresting hook AVIONICS bobweight camber CAP station capability characteristics chart cockpit configuration CONSTRAINT cost cylinder drag duct dynamic effect ejection ejection seat engine envelope Escape System fighter fire control system Frankford Arsenal frequency fuel fuselage gain margin handling qualities high speed horizontal tail hydraulic actuator improved increase initial inlet intercept interceptor intruder landing gear lead computing leading edge LEADING EDGE EXTENSION LINE load factor loop Mach number maintenance maximum speeds minimize MISSILE LAUNCH COMPUTER Northrop nose gear parameter performance pilot PLATFORM pound of weight RADAR ratio reduced result retract rocket catapult seat shock strut short transverse grain SHOT PEENING shown skins spar stability stress corrosion cracking structure subsonic supersonic takeoff TARGETS tensile stresses transonic turn rate USAF WEAPON DELIVERY weight saved wind tunnel wind tunnel tests wing
Bibliografische Informationen
| Titel | Northrop F-5 case study in aircraft design Case Studies AIAA professional study series |
| Autor | William G. Stuart |
| Verlag | Northrop Corporation, 1978 |
| Original von | University of Michigan |
| Digitalisiert | 14. Dez. 2007 |
| Länge | 219 Seiten |
| Zitat exportieren | BiBTeX EndNote RefMan |