Charts And Approximate Formulas For The Estimation Of Aeroelastic Effects On The Loading Of Swept And Unswept Wings
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Charts and Approximate Formulas for the Estimation of Aeroelastic Effects on the Loading of Swept and Unswept Wings
Charts are presented for the estimation of aeroelastic effects on spanwise lift distribution, lift-curve slope, aerodynamic career, and damping in roll of swept and unswept wings at subsonic and supersonic speeds. Some design considerations brought out by the results of this paper are discussed.
Report - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
language: en
Publisher:
Release Date: 1952