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Wind-tunnel Investigation of a Revised Horizontal Tail Surface for the Grumman TBF-1 Airplane
John W. McKee
Robert B. Liddell
出版
National Advisory Committee for Aeronautics
, 1943
URL
http://books.google.com.hk/books?id=8mTFEAlaz5MC&hl=&source=gbs_api
EBook
FULL_PUBLIC_DOMAIN
註釋
An investigation was made in the LMAL 7- by 10-foot tunnel of the aerodynamic characteristics of a revised 0.5-scale model of the Grumman TBF-1 left horizontal tail surface. The investigation was undertaken to determine if a horizontal tail surface with a large overhang would reduce the high stick forces in maneuvers that the airplane had with the original horn-balanced elevator, without appreciably affecting the longitudinal stability characteristics of the airplane.
