Method separates aerodynamic and structural calculations, making it possible to use either theoretical or experimental determinations of spanwise loading and to account for induction effects; method can be used to solve usual aerodynamic problems arising in longitudinal and lateral stability and control and to provide structural design criteria.
Superposition method for calculating aeroelastic behavior of swept wings
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 18 , n 8
1951
12 pages
Aufsatz (Zeitschrift)
Englisch
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