This report reviews existing information regarding the behaviour of the local aerodynamic centres of aerofoils, with a view to exposing the more important gaps in our knowledge, and, indicating the lines along which future ...
This report, which is presented in two parts, develops an approximate method of estimating the effect of structural deformability on the manoeuvre point of an aircraft. The introduction outlines the scope of the complete ...
PART I Estimation of the Effect of Longitudinal Elastic Camber on Trim and Manoeuvrability of Slender Aircraft. An approximate method of estimating the effect of aeroelasticity on the longitudinal trim and quasi-steady ...
This Report presents a matrix formulation of a method which employs influence coefficients to solve static aeroelastic problems. Linear structural characteristics are assumed and the aerodynamic loading, including that due ...
This Report provides, in tabular form, resumes of the contents of reports which give comparative theoretical and experimental aerodynamic loading data and, in some cases, structural deformation data, relevant to zero- and ...
Foreword (1961). Parts I and II of this R. & M. were written as separate Reports in 1958 and 1960. They deal with two stages of an exploratory investigation into the stability, control and response characteristics of ...