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Effects of Wing Position and Fuselage Size on the Low-speed Static and Rolling Stability Characteristics of a Delta-wing Model
Alex Goodman
David F. Thomas
出版
National Advisory Committee for Aeronautics
, 1954
URL
http://books.google.com.hk/books?id=4-y_LnH4Qy0C&hl=&source=gbs_api
EBook
FULL_PUBLIC_DOMAIN
註釋
An investigation was made to determine the effects of wing position and fuselage size on the low-speed static and rolling stability characterististics of airplane models having a triangular wing and vertical tail surfaces.