Critical hypersonic aerothermodynamic phenomena

被引:179
作者
Bertin, JJ [1 ]
Cummings, RM
机构
[1] Rice Univ, Dept Mech Engn & Mat Sci, Houston, TX 77251 USA
[2] USAF Acad, Dept Aeronaut, Colorado Springs, CO 80840 USA
关键词
hypersonic; ground testing; CFD; flight testing; boundary-layer transition;
D O I
10.1146/annurev.fluid.38.050304.092041
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The challenges in understanding hypersonic flight are discussed and critical hypersonic aerothermodynamics issues are reviewed. The ability of current analytical methods, numerical methods, ground testing capabilities, and flight testing approaches to predict hypersonic flow are evaluated. The areas where aerothermodynamic shortcomings restrict our ability to design and analyze hypersonic vehicles are discussed, and prospects for future capabilities are reviewed. Considerable work still needs to be done before our understanding of hypersonic flow will allow for the accurate prediction of vehicle flight characteristics throughout the flight envelope from launch to orbital insertion.
引用
收藏
页码:129 / 157
页数:29
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