×
模态框(Modal)标题
在这里添加一些文本
Close
Close
Submit
Cancel
Confirm
×
模态框(Modal)标题
×
CJA
中文
导航
Home
Journal
Editorial Board
Archive
Guide for Authors
Academic Quality
Advertising Services |
Subscriptions |
Home
Journal
Editorial Board
Archive
Guide for Authors
中文
CJA
A NUMERICAL SOLUTION OF THE SHOCK-TURBULENT BOUNDARY LAYER INTERACTION OVER A COMPRESSION CORNER FOR SUPERSONIC FLOW
Cao Qipeng
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 1983, (
4
): 11 -19 .