Numerical study on the influence of wall temperature gradient on aerodynamic characteristics of low aspect ratio flying wing configuration.

Lin, Peng; Liu, Xueqiang; Xiong, Neng; Wang, Xiaobing; Shang, Ma; Liu, Guangyuan; Tao, Yang.

Afiliação

Lin P; College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, No. 29 Yudao Street, Nanjing, 210016, China.
Liu X; Hunan Lingxiang Maglev Technology Co., Ltd, Changsha, 410004, China.
Xiong N; College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, No. 29 Yudao Street, Nanjing, 210016, China.
Wang X; China Aerodynamics Research and Development Center, High Speed Aerodynamic Institute, Mianyang, 621000, China.
Shang M; China Aerodynamics Research and Development Center, High Speed Aerodynamic Institute, Mianyang, 621000, China.
Liu G; China Aerodynamics Research and Development Center, High Speed Aerodynamic Institute, Mianyang, 621000, China.
Tao Y; China Aerodynamics Research and Development Center, High Speed Aerodynamic Institute, Mianyang, 621000, China.

Sci Rep ; 11(1): 16295, 2021 Aug 11.

Article em En | MEDLINE | ID: mdl-34381068

Texto completo: 1 Base de dados: MEDLINE Idioma: En Ano de publicação: 2021 Tipo de documento: Article

Texto completo: 1 Base de dados: MEDLINE Idioma: En Ano de publicação: 2021 Tipo de documento: Article