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A Piloted Simulator Investigation of Ground Effect on the Landing Maneuver of a Large, Tailless, Delta-wing Airplane
C. Thomas Snyder
Fred J. Drinkwater
A. David Jones
出版
National Aeronautics and Space Administration
, 1970
URL
http://books.google.com.hk/books?id=MKMHSj7zWpAC&hl=&source=gbs_api
EBook
FULL_PUBLIC_DOMAIN
註釋
The influence of ground effect on the landing flare characteristics of a supersonic transport airplane (SST) was investigated in a fixed cockpit simulator. Simulations of an ogee-modified delta-wing F5D-1 airplane and a subsonic jet transport were used for evaluating the simulator and as a reference configurations during landing comparisons. Dynamic responses of the SST to seven different ground-effect models during controls-fixed and constant-attitude descents are also presented, followed by piloted subjective assessments. A summary of ground effects on delta-like wings is included in the appendixes.
