This chapter contains sections titled:
Introduction
Maximum Take‐Off Weight Estimation
Wing Area and Engine Sizing
Design Examples
Problems
References
Preliminary Design
2012-10-26
67 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
aircraft preliminary design phase, parameters direct on design phase , solved design examples, MTOW (WTO) and wing reference (S) and engine P , aircraft performance criterion loiter, and endurance parameter , preliminary design, employing the outcomes of a calculation , wing area and engine sizing, wing reference area determination , trial‐and‐error in determining maximum take‐off weight of aircraft , air craft performance requirements , aircrafts, techniques of obtaining first estimate of the MTOW , cruise weight fraction for jet aircraft
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