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机译:Investigations on the aerothermoelastic properties of composite laminated cylindrical shells with elastic boundaries in supersonic airflow based on the Rayleigh-Ritz method
Harbin Inst Technol, Sch Astronaut, POB 137, Harbin 150001, Heilongjiang, Peoples R China;
Harbin Engn Univ, Coll Aerosp & Civil Engn, Harbin 150001, Heilongjiang, Peoples R China;
Aerothermoelastic properties; Composite laminated cylindrical shell; Elastic boundary conditions; Rayleigh-Ritz method; Characteristic orthogonal polynomials;