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
ACTION actuator additional aileron aircraft airplane altitude aluminum analysis angle of attack characteristics chart chute combat COMPUTER configuration considerable considered CONSTRAINT control system cost cracking DATA deflection DETECTION direct DISTANCE door drag dynamic edge effect ejection element engine ENVELOPE factor fighter final fire control flap flight force frequency FUEL fuselage gain gear ground higher hydraulic improved increase initial inlet intercept landing LAUNCH leading lift limit LINE load Mach number maintain maintenance major maneuvering MARGIN material maximum mechanical minimize MISSILE Northrop nose operation original performance pilot position possible pound presented primary problem production qualities RADAR radius range ratio reduced result retract rocket ROLL saved seat selected shown shows skins spar speed stability STATION stress corrosion structure strut supersonic surface tail turn rate utilized WEAPON weight wing
Bibliografische Informationen
| Titel | Northrop F-5 Case Study in Aircraft Design AIAA professional study series, American Institute of Aeronautics and Astronautics Case Studies Library of flight |
| Autor/in | William G. Stuart |
| Verlag | American Institute of Aeronautics and Astronautics, 1978 |
| Original von | University of Michigan |
| Digitalisiert | 14. Dez. 2007 |
| ISBN | 1563473097, 9781563473098 |
| Länge | 219 Seiten |
| Zitat exportieren | BiBTeX EndNote RefMan |