THE EFFECT OF COMPRESSIBILITY FOR DISPLACEMENT NOISE FROM THE HELICOPTER ROTOR

THE EFFECT OF COMPRESSIBILITY FOR DISPLACEMENT NOISE FROM THE HELICOPTER ROTOR

The problem of noise generation of rotor due to the thickness of blades - displacement noise is considered. The method of calculating the displacement noise, which is based on linear acoustic theory for the changes in the effective thickness of the blade over time due to the compressibility of the f...

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Bibliographic Details
Main Authors: B. S. Kritskiy, R. M. Mirgazov, A. A. Nikolskiy
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2016-11-01
Series:Naučnyj Vestnik MGTU GA
Subjects:
вертолет
несущий винт
шум вытеснения
лопасть
уровень звукового давления
сжимаемость
Online Access:https://avia.mstuca.ru/jour/article/view/124
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spelling doaj-a6a3a66169cc42049eb040b095f83c572021-07-28T21:00:31ZrusMoscow State Technical University of Civil Aviation Naučnyj Vestnik MGTU GA2079-06192542-01192016-11-012124550124THE EFFECT OF COMPRESSIBILITY FOR DISPLACEMENT NOISE FROM THE HELICOPTER ROTORB. S. Kritskiy0R. M. Mirgazov1A. A. Nikolskiy2ЦАГИ им. проф. Н.Е. ЖуковскогоЦАГИ им. проф. Н.Е. ЖуковскогоЦАГИ им. проф. Н.Е. ЖуковскогоThe problem of noise generation of rotor due to the thickness of blades - displacement noise is considered. The method of calculating the displacement noise, which is based on linear acoustic theory for the changes in the effective thickness of the blade over time due to the compressibility of the flow are described.https://avia.mstuca.ru/jour/article/view/124вертолетнесущий винтшум вытеснениялопастьуровень звукового давлениясжимаемость
collection DOAJ
language Russian
format Article
sources DOAJ
author B. S. Kritskiy
R. M. Mirgazov
A. A. Nikolskiy
spellingShingle B. S. Kritskiy
R. M. Mirgazov
A. A. Nikolskiy
THE EFFECT OF COMPRESSIBILITY FOR DISPLACEMENT NOISE FROM THE HELICOPTER ROTOR
Naučnyj Vestnik MGTU GA
вертолет
несущий винт
шум вытеснения
лопасть
уровень звукового давления
сжимаемость
author_facet B. S. Kritskiy
R. M. Mirgazov
A. A. Nikolskiy
author_sort B. S. Kritskiy
title THE EFFECT OF COMPRESSIBILITY FOR DISPLACEMENT NOISE FROM THE HELICOPTER ROTOR
title_short THE EFFECT OF COMPRESSIBILITY FOR DISPLACEMENT NOISE FROM THE HELICOPTER ROTOR
title_full THE EFFECT OF COMPRESSIBILITY FOR DISPLACEMENT NOISE FROM THE HELICOPTER ROTOR
title_fullStr THE EFFECT OF COMPRESSIBILITY FOR DISPLACEMENT NOISE FROM THE HELICOPTER ROTOR
title_full_unstemmed THE EFFECT OF COMPRESSIBILITY FOR DISPLACEMENT NOISE FROM THE HELICOPTER ROTOR
title_sort effect of compressibility for displacement noise from the helicopter rotor
publisher Moscow State Technical University of Civil Aviation
series Naučnyj Vestnik MGTU GA
issn 2079-0619
2542-0119
publishDate 2016-11-01
description The problem of noise generation of rotor due to the thickness of blades - displacement noise is considered. The method of calculating the displacement noise, which is based on linear acoustic theory for the changes in the effective thickness of the blade over time due to the compressibility of the flow are described.
topic вертолет
несущий винт
шум вытеснения
лопасть
уровень звукового давления
сжимаемость
url https://avia.mstuca.ru/jour/article/view/124
work_keys_str_mv AT bskritskiy theeffectofcompressibilityfordisplacementnoisefromthehelicopterrotor
AT rmmirgazov theeffectofcompressibilityfordisplacementnoisefromthehelicopterrotor
AT aanikolskiy theeffectofcompressibilityfordisplacementnoisefromthehelicopterrotor
AT bskritskiy effectofcompressibilityfordisplacementnoisefromthehelicopterrotor
AT rmmirgazov effectofcompressibilityfordisplacementnoisefromthehelicopterrotor
AT aanikolskiy effectofcompressibilityfordisplacementnoisefromthehelicopterrotor
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