Flight Vehicle Performance and Aerodynamic Control is designed to serve as a text for either an 11-week or a 16-week course at the sophomore level. It explains typical methods used to estimate aircraft performance, the theoretical basis of these methods, and how various parameters derived from the aircraft geometry can be used to estimate the requirements of control surfaces and the aerodynamic forces required to actuate these surfaces.
Flight Vehicle Lift-Drag Characteristics
2001-01-01
27 pages
Article/Chapter (Book)
Electronic Resource
English
Lift and drag characteristics of a cabin monoplane determined in flight
Engineering Index Backfile | 1931
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