Effect of reflex camber on the aerodynamic characteristics of a highly tapered moderately swept-back wing at Reynolds numbers up to 8,000,000

D. William Conner.
Washington D.C. : National Advisory Committee for Aeronautics, 1947.
Physical description
10, [13] p. : ill. ; 28 cm.
Technical note (United States. National Advisory Committee for Aeronautics) ; 1212.

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Librarian view | Catkey: 9121466