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Aeroacoustics of Shallow Cylindrical Cavities with Specific Application to the Inter-wheel Region of Aircraft Nose Landing Gears

机译：浅圆柱空腔的空气声学，具有特定应用的飞机鼻落齿轮

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作者
McCarthy, Philip W.;
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作者单位

University of Toronto (Canada).;

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授予单位 University of Toronto (Canada).;
学科
学位 Ph.D.
年度 2020
页码 190 p.
总页数 190
原文格式 PDF
正文语种 eng
中图分类 AAI27670784;
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1. Parameter Optimization of Nose Landing Gear Considering Both Take-off and Landing Performance of Catapult Take-off Carrier-Based Aircraft [J] . Zhang Ming, Nie Hong, He Zhihang 南京航空航天大学学报（英文版） . 2016,第002期

机译：同时考虑弹射起飞航母飞机起降性能的前起落架参数优化
2. Design and Analysis Aircraft Nose and Nose Landing Gear [J] . Rajesh A, Abhay BT Journal of Aeronautics & Aerospace Engineering . 2015,第2期

机译：飞机机头和机鼻起落架的设计与分析
3. Numerical simulation of aeroacoustic noise from landing gear and rectangular cavity [J] . Guo Zhifei, Liu Peiqing, Zhang Jin, Proceedings of the Institution of Mechanical Engineers . 2020,第7期

机译：着陆齿轮和矩形空气声噪声的数值模拟
4. Application of FUN3D Solver for Aeroacoustics Simulation of a Nose Landing Gear Configuration [C] . Veer N. Vatsa, David P. Lockard, Mehdi R. Khorrami 17th AIAA/CEAS aeroacoustics conference 2011 . 2011

机译：FUN3D解算器在鼻子起落架构型的航空声学仿真中的应用
5. Aeroacoustic characterization of scaled canonical nose landing gear configurations [D] . Zawodny, Nikolas S. 2013

机译：比例规范的前起落架配置的航空声学特性
6. Determining Wheel Forces and Moments on Aircraft Landing Gear with a Dynamometer Sensor [O] . Jaroslaw Pytka, Piotr Budzyński, Tomasz Łyszczyk, 2020

机译：使用测力计传感器确定飞机起落架上的车轮力和力矩
7. Comparing flyover noise measurements to full-scale nose landing gear wind tunnel experiments for regional aircraft [O] . Merino Martinez, R., Neri, Eleonora, Snellen, M., 2017

机译：将飞越噪声测量结果与支线飞机的全面前起落架风洞实验进行比较
8. Application of FUN3D Solver for Aeroacoustics Simulation of a Nose Landing Gear Configuration [R] . Vatsa, V. N., Lockard, D. P., Khorrami, M. R. 2011

机译：FUN3D求解器在鼻型起落架构件气动声学仿真中的应用

Aeroacoustics of Shallow Cylindrical Cavities with Specific Application to the Inter-wheel Region of Aircraft Nose Landing Gears

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