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The Next Generation of High-Speed Dynamic Stability Wind Tunnel Testing (Invited)

机译:下一代高速动态稳定性风洞测试(已邀请)

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摘要

Throughout industry, accurate measurement and modeling of dynamic derivative data at high-speed conditions has been an ongoing challenge. The expansion of flight envelopes and non-conventional vehicle design has greatly increased the demand for accurate prediction and modeling of vehicle dynamic behavior. With these issues in mind, NASA Langley Research Center (LaRC) embarked on the development and shakedown of a high-speed dynamic stability test technique that addresses the longstanding problem of accurately measuring dynamic derivatives outside the low-speed regime. The new test technique was built upon legacy technology, replacing an antiquated forced oscillation system, and greatly expanding the capabilities beyond classic forced oscillation testing at both low and high speeds. The modern system is capable of providing a snapshot of dynamic behavior over a periodic cycle for varying frequencies, not just a damping derivative term at a single frequency.
机译:在整个行业中,高速条件下动态导数数据的精确测量和建模一直是一个挑战。飞行范围的扩大和非常规车辆设计极大地增加了对车辆动态行为的准确预测和建模的需求。考虑到这些问题,美国宇航局兰利研究中心(LaRC)着手开发和淘汰了高速动态稳定性测试技术,该技术解决了长期以来一直在低速范围之外精确测量动态导数的问题。新的测试技术建立在传统技术的基础上,取代了过时的强制振荡系统,极大地扩展了其在低速和高速下的能力,超越了传统的强制振荡测试。现代系统能够为变化的频率提供周期性周期内动态行为的快照,而不仅仅是单个频率上的阻尼导数项。

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