Shock-stable flux scheme for predicting aerodynamic heating load of hypersonic airliners
Crossref DOI link: https://doi.org/10.1007/s11433-018-9347-6
Published Online: 2019-03-27
Published Print: 2019-08
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Qu, Feng
Kong, WeiXuan
Sun, Di
Bai, JunQiang
Text and Data Mining valid from 2019-03-27
Article History
Received: 30 July 2018
Accepted: 24 December 2018
First Online: 27 March 2019