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CHAPTER 5 WING DESIGN - unina.it
wpage.unina.itWing Design 1 CCHHAAPPTTEERR 55 WWIINNGG DDEESSIIGGNN 5.1. Introduction In chapter 4, aircraft preliminary design – the second step in design process – was introduced. Three parameters were determined during preliminary design, namely: aircraft maximum takeoff
Optimization Techniques - Sam Houston State University
www.shsu.eduall-wing design was the one that maximized range, when, in fact, it minimized range. In this chapter we introduce some of the same optimization techniques applied to an analy-sis of the Stealth bomber project. We develop tools designed to maximize profits or minimize costs. Fortunately, the mathe-matical functions we deal with in this chapter ...