Numerical treatment of influence of aeroelastic deformations is carried out for subcritical speed range; method to calculate deformations of wing is based on Superposition Method for Calculating Aeroelastic Behavior of Swept Wings, R.B.Brown et al, indexed in Engineering Index 1951 p 45; comparison of numerical results with those of another more exact method which prove reliability of present method; stability and control of aircraft are only slightly affected by aeroelastic deformation.
Influence of aeroelasticity on longitudinal stability of swept wing subsonic transport aircraft
AGARD -- Report
1961
40 pages
Report
Englisch
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