Computational Verification of Acoustic Damping in High-Enthalpy Environments

被引:2
|
作者
Wagnild, Ross [1 ]
Candler, Graham V. [2 ]
机构
[1] Sandia Natl Labs, Aerosci Dept, Albuquerque, NM 87123 USA
[2] Univ Minnesota, Dept Aerosp Engn & Mech, Minneapolis, MN 55455 USA
关键词
SOUND;
D O I
10.2514/1.J052802
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The motivation for studying acoustic propagation in high enthalpy environments lies partially in the role that acoustics play in promoting laminar-turbulent boundary-layer transition. At high speeds, boundary-layer transition on slender-body vehicles is primarily due to Mack's second-mode instability. If the growth of disturbances is sufficiently reduced, then laminar- turbulent boundary-layer transition could be delayed or prevented. In many cases, maintaining laminar flow over a high-speed vehicle is beneficial because a laminar boundary layer exerts significantly less heating and shear forces on the vehicle than a turbulent boundary layer. Accurately capturing the physics of transition would allow for a more precise prediction of the transition location. Less uncertainty in the transition location would then allow for optimization of thermal protection systems and design of high-speed vehicles. Thus, it is important to understand the interaction of an acoustic wave with a high-enthalpy flow environment.
引用
收藏
页码:2615 / 2618
页数:4
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