Method of transfer matrices is used in study of response of flexible airplanes to random vertical gusts; nonhomogeneous and homogeneous gust fields can be treated within present framework; formulation is carried out in case of slender wing with nonuniform sweep angle, which is possible configuration for large supersonic transports; since bending moment, torsional moment, and shear are treated directly as unknowns rather than indirectly obtained from differentiating deflections, method yields more accurate assessment of random stress levels.
Transfer matrix representation of flexible airplanes in gust response study
J Aircraft
Journal of Aircraft ; 2 , n 2
1965
6 pages
Aufsatz (Zeitschrift)
Englisch
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