The formulation of an influence-coefficient method for determining static aeroelastic effects : and its application to a slender aircraft in symmetric flight at M = 2.2 /

Bibliographic Details

Main Author:	Taylor, A. S.
Other Authors:	Eckford, Duncan John
Format:	Book
Language:	English
Published:	London : H.M.S.O., 1969.
Series:	Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 3573.
Subjects:	Aeroelasticity. Aerodynamics, Supersonic. Supersonic transport planes.