The invention relates to a pneumatic elastic analytical method, and provides a pneumatic elastic mechanical characteristic analytical method of a hypersonic speed aircraft in thermal environment. According to the method, the
piston theory is used for carrying out
frequency domain nonsteady aerodynamic calculation on a full-aircraft finite
element model of the hypersonic speed aircraft; on the basis, the pneumatic
thermal effect on the model in the hypersonic speed thermal environment is considered; the weak
coupling effect of pneumatic thermal input in aerodynamic input and elastic force input is ignored; only the structure temperature steady-state characteristics under the pneumatic
thermal load effect are considered; after the steady aerodynamic calculation, the thermal flux density on the surface of the aircraft is obtained by adopting a reference
enthalpy method; further, the steady temperature distribution on the surface of the aircraft is calculated; the practical equivalent
rigidity matrix of the structure at the moment is obtained; and the critical
flutter speed is calculated by an
engineering method. The pneumatic elastic mechanical characteristic analytical method has the advantages that the pneumatic elastic
analytical problem of the hypersonic speed aircraft in the pneumatic thermal environment is solved, and the pneumatic elastic performance of the hypersonic speed aircraft is improved through
flutter speed analysis.