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Airborne weaponry noise measurements

机译:机载武器噪声测量

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摘要

Many aircraft noise models exist that estimate noise levels from military aircraft operations nearairbases, along training routes, and within special use airspace, but these models do not includecontributions to the noise by air gunnery and air fired missile operations. A new air-weaponrymodel is being developed to assess noise from these unique military operations. This paperdescribes the initial field measurements used to characterize air-weaponry noise sources and toevaluate propagation algorithms. Air gunnery noise data were collected from helicopter andfixed-wing aircraft operations. Missile launch noise data were collected from helicopteroperations. For the air gunnery noise, important aspects of time-dependent waveforms andspectral descriptions for muzzle blasts and ballistic waves are discussed along with theirdirectivity patterns. This analysis demonstrates that the positive impulse is the most stablemetric for describing the muzzle blast. The peak is best for describing the ballistic wave; and theCSEL is best for the missile launch and thrust noise. For the propagation algorithm, the lineargeometric theory of diffraction agrees well with the measured data. The development of an airweaponry model will be described in a companion paper.
机译:存在许多飞机噪声模型,这些模型可估计来自空军基地,沿训练路线以及特殊用途空域内的军用飞机运行的噪声水平,但是这些模型不包括空中炮兵和空中导弹运行对噪声的贡献。正在开发一种新的空中武器模型,以评估这些独特军事行动产生的噪声。本文描述了用于表征航空武器噪声源和评估传播算法的初始现场测量。航空炮噪声数据是从直升机和固定翼飞机的运营中收集的。导弹发射噪声数据是从直升机作战中收集的。对于航空炮声,讨论了与时间有关的波形的重要方面以及炮口爆炸和弹道波的频谱描述及其方向性模式。该分析表明,正冲量是描述枪口爆炸的最稳定指标。峰值最适合描述弹道。 CSEL最适合导弹的发射和推力噪声。对于传播算法,衍射的线性几何理论与实测数据非常吻合。航空兵模型的开发将在随附的论文中进行描述。

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