摘要: The presence of shock wave boundary-layer interactions (SBLI) on thin and compliant panels adds complexities to vehicle design. Shock waves impose an adverse pressure gradient across it, leading to high loads and resulting in a se... 展开
作者 | Kartika Ahuja Srisha Rao MV | ||
---|---|---|---|
作者单位 | |||
文集名称 | 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2023 | ||
出版年 | 2023 | ||
会议名称 | AIAA International Space Planes and Hypersonic Systems and Technologies Conference | ||
卷/页码 | Vol. 2 / 858-868 | 开始页/总页数 | 00000858 / 11 |
会议地点 | Bengaluru(IN) | 会议年/会议届次 | 2023 / 25th |
馆藏号 | P2400014 |