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The Effect of High Wing Loading on Landing Technique and Distance, with Experimental Data for the B-26 Airplane
F. B. Gustafson
William J. O'Sullivan
出版
National Advisory Committee for Aeronautics
, 1945
URL
http://books.google.com.hk/books?id=M1T_nuPbb7kC&hl=&source=gbs_api
EBook
FULL_PUBLIC_DOMAIN
註釋
Summary: An analysis of the effect of wing loading on the landing flare (that is, the leveling-off part of the landing) indicated an important effect on landing technique and distance. In order to check this analysis, flight tests were made with a Martin B-26 airplane loaded to 50 pounds per square foot. It was found that, for reasonable accuracy and safety, the pilots used power to maintain the desired speed margin and to limit the rate of descent at the start of the flare to about 25 feet per second.
