首页> 外文会议>AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition >Measurements of the Interaction of an Upstream Laser Perturbation with a Forward-Facing Cavity
【24h】

Measurements of the Interaction of an Upstream Laser Perturbation with a Forward-Facing Cavity

机译:测量具有正向腔的上游激光摄动的相互作用

获取原文

摘要

The laser perturber is a tool to be used for receptivity studies in the Boeing/AFOSR Mach-6 Quiet Tunnel. To demonstrate that the laser perturber is functioning correctly, it is tested with a forward-facing cavity. Results are similar to previous studies by Ladoon and Segura in a Mach-4 quiet tunnel. The cavity base pressure fluctuations are nearly quiescent at shallow cavity depths. When a freestream perturbation interacts with the forward facing cavity, the cavity base pressure experiences oscillations that decay exponentially. The measured cavity resonance frequency matches the theoretical cavity resonance frequency to within 6%. The measured cavity response appears to be initiated by the acoustic disturbance that results from the laser-generated perturbation. The damping characteristics of the forward-facing cavity are also examined. For cavities with similar resonant frequencies, the damping constants can differ by almost an order of magnitude. However, cavities with similar non-dimensional depths have similar damping constants.
机译:激光干扰器是用于波音/ AFOSR Mach-6静音隧道中接受性研究的工具。为了证明激光干扰器工作正常,使用了朝前的腔体对其进行了测试。结果与Ladoon和Segura在Mach-4安静隧道中的先前研究相似。在浅腔深度处,腔基础压力波动几乎是静止的。当自由流扰动与朝前的空腔相互作用时,空腔的基础压力将经历呈指数衰减的振荡。测得的腔共振频率与理论腔共振频率相匹配,在6%之内。测得的腔响应似乎是由激光产生的扰动引起的声干扰引起的。还检查了朝前腔体的阻尼特性。对于谐振频率相似的腔,阻尼常数可能相差近一个数量级。但是,具有类似无量纲深度的型腔具有类似的阻尼常数。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号