单个螺旋桨声源噪声评估：基于全尺寸 eVTOL 飞行测试测量
Individual Propeller Source Noise Assessment from Full-Scale eVTOL Flight Test Measurements
打开原文本文通过飞行测试和模拟分析，评估了 eVTOL 飞机单个螺旋桨的噪声源特性，揭示了分布式推进系统中噪声的复杂性。研究结果有助于理解 eVTOL 噪声控制的关键因素，对适航审定和噪声管理具有参考价值。依据来源摘要
以下展示完整原文，全文中文翻译尚未生成。
Document ID
20260000259
Acquisition Source
Langley Research Center
Document Type
Accepted Manuscript (Version with final changes)
Authors
Kyle A Pascioni
(Langley Research Center Hampton, United States)
Austin D Thai
(Joby Aviation)
Jeremy J Bain
(Joby Aviation)
Date Acquired
January 9, 2026
Publication Date
January 7, 2026
Publication Information
Publication: AIAA Journal of Aircraft
Publisher: American Institute of Aeronautics and Astronautics
e-ISSN: 1533-3868
Subject Category
Funding Number(s)
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
External Peer Committee
Keywords
来源：NASA NTRS先进空中交通原始技术报告 · ntrs.nasa.gov