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Research on Calculation Method of Aerodynamic Parameters of Supersonic Probe Based on Gas Compressibility Factor

ZHONG Jingjun HUANG Gangfeng WU Wanyang KAN Xiaoxu

热科学学报（英文版）2022，Vol.31Issue(1)：111-119,9.

Research on Calculation Method of Aerodynamic Parameters of Supersonic Probe Based on Gas Compressibility Factor

ZHONG Jingjun ¹HUANG Gangfeng ¹WU Wanyang ¹KAN Xiaoxu¹

作者信息

1. Merchant Marine College,Shanghai Maritime University,1550 Haigang Avenue,Pudong District,Shanghai 201306
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摘要

关键词

supersonic flow/probe/gas compressible factor/aerodynamic parameter/error analyses

Key words

supersonic flow/probe/gas compressible factor/aerodynamic parameter/error analyses

引用本文复制引用

ZHONG Jingjun,HUANG Gangfeng,WU Wanyang,KAN Xiaoxu..Research on Calculation Method of Aerodynamic Parameters of Supersonic Probe Based on Gas Compressibility Factor[J].热科学学报（英文版）,2022,31(1):111-119,9.

基金项目

This study was co-supported by the National Natural Science Foundation of China (No.51906134 and 51436002). （No.51906134 and 51436002）

热科学学报（英文版）

OACSCDEISCI

ISSN：1003-2169

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