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Large-scale Wind-tunnel Tests of Descent Performance of an Airplane Model with a Tilt Wing and Differential Propeller Thrust
Wallace H. Deckert
V. Robert Page
Stanley O. Dickinson
出版
National Aeronautics and Space Administration
, 1964
URL
http://books.google.com.hk/books?id=mMG-HLCIFWQC&hl=&source=gbs_api
EBook
FULL_PUBLIC_DOMAIN
註釋
Tests were conducted to determine the wing stall, performance, and longitudinal stability and control characteristics of a large model of a V/STOL tilt-wing transport aircraft. The scope of the tests was limited primarily to the low-speed transitional regime.
