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Linearized Lifting-surface Theory for Swept-back Wings with Slender Plan Forms
Harvard Lomax
Max A. Heaslet
出版
National Advisory Committee for Aeronautics
, 1949
URL
http://books.google.com.hk/books?id=ppkpS5yhu2kC&hl=&source=gbs_api
EBook
FULL_PUBLIC_DOMAIN
註釋
The spanwise and chordwise distribution of loading, the lift, and the induced drag of a swept-back wing of slender plan form are developed by means of linearized lifting-surface theory. The results are applicable for all free-stream Mach numbers. The term slender implies that the ratio of the reduced span to over-all length of the wing is small.
