The invention relates to a stability
analysis method and
system for a boundary layer of a high-
enthalpy ablated wall surface, and is applied to the technical field of
aerospace, and the method comprises the steps: taking a Landau-Teller equation and a
chemical reaction rate equation as source items, constructing a
control equation, and solving the
control equation to obtain a steady laminar flow field; analyzing the steady laminar flow field by using LST to obtain a
transmission coefficient eigenvalue; if the first
modal time scale and the second
modal time scale are greater than or equal to 1, correcting the first
modal time scale and the second modal time scale based on the roughness of each position of the wall surface of the high-speed aircraft, and constructing a first modal linear operator and a second modal linear operator; further constructing NPSE, and solving to obtain an NPSE result; when an NPSE result is decomposed and linearized according to Fourier subharmonics, a
coupling source item of a
subharmonic equation is constructed according to a second modal linear operator, secondary
instability analysis is carried out, and a transition initial position and the amplitude and frequency of disturbance development are obtained. And the accuracy of stability analysis can be improved.