Taylor, A. S., & Eckford, D. J. (1969). 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. H.M.S.O..
Chicago Style (17th ed.) CitationTaylor, A. S., and Duncan John Eckford. 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. London: H.M.S.O., 1969.
MLA (9th ed.) CitationTaylor, A. S., and Duncan John Eckford. 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. H.M.S.O., 1969.
Warning: These citations may not always be 100% accurate.