The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Feb. 04, 2025

Filed:

May. 31, 2023
Applicant:

Beihang University, Beijing, CN;

Inventors:

Zhifan Ye, Beijing, CN;

Jin Zhao, Beijing, CN;

Zhihui Li, Beijing, CN;

Dongsheng Wen, Beijing, CN;

Guice Yao, Beijing, CN;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G06F 30/28 (2020.01); G06F 30/15 (2020.01); G06F 111/10 (2020.01); G06F 119/08 (2020.01);
U.S. Cl.
CPC ...
G06F 30/28 (2020.01); G06F 30/15 (2020.01); G06F 2111/10 (2020.01); G06F 2119/08 (2020.01);
Abstract

A multi-scale prediction method for an ablation behavior of a hypersonic aircraft heat resistant structure, includes inputting hypersonic inflow far field boundary conditions into a macro CFD solver to perform numerical simulation of the external flow field of a hypersonic aircraft; extracting the mass fraction and temperature distribution of wall surface components; obtaining an msd.txt file and an atomic path file recording the mean square displacement data through a micro RMD solver; obtaining the ratio of mass loss rate to material density, namely, the ablation retreating rate using the MSD method and Fick's law; inputting it into a CFD solver for performing grid reconstruction and transient calculation to obtain the transient variation in the external flow field of a hypersonic aircraft along the ablation retreating of the aircraft wall surface.


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