PROPELLERLAERM BEI UNTERSCHALIBLATTSPITZENMACHZAHLEN UMFANGSKRAFT UND AXIALKRAFT. right brace Propeller Noise at Subsonic Blade Tip Speeds, Torque and Thrust Force

Roland Stuff

PROPELLERLAERM BEI UNTERSCHALIBLATTSPITZENMACHZAHLEN UMFANGSKRAFT UND AXIALKRAFT. right brace Propeller Noise at Subsonic Blade Tip Speeds, Torque and Thrust Force

Translated title of the contribution: ..

Roland Stuff^*

^*Corresponding author for this work

King Fahd University of Petroleum & Minerals

Research output: Contribution to journal › Article › peer-review

Abstract

The sound generation due to propeller blade forces is described by an acceleration source. Closed form solutions are presented for the sound field of a propeller in yaw with asymmetric disk loading.

Translated title of the contribution	..
Original language	German
Journal	Mitteilung - Deutsche Forschungs- und Versuchsanstalt fuer Luft- und Raumfahrt
State	Published - 1982

ASJC Scopus subject areas

General Engineering

Cite this

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title = "PROPELLERLAERM BEI UNTERSCHALIBLATTSPITZENMACHZAHLEN UMFANGSKRAFT UND AXIALKRAFT. right brace Propeller Noise at Subsonic Blade Tip Speeds, Torque and Thrust Force",

abstract = "The sound generation due to propeller blade forces is described by an acceleration source. Closed form solutions are presented for the sound field of a propeller in yaw with asymmetric disk loading.",

author = "Roland Stuff",

year = "1982",

language = "German",

journal = "Mitteilung - Deutsche Forschungs- und Versuchsanstalt fuer Luft- und Raumfahrt",

}

TY - JOUR

T1 - PROPELLERLAERM BEI UNTERSCHALIBLATTSPITZENMACHZAHLEN UMFANGSKRAFT UND AXIALKRAFT. right brace Propeller Noise at Subsonic Blade Tip Speeds, Torque and Thrust Force

AU - Stuff, Roland

PY - 1982

Y1 - 1982

N2 - The sound generation due to propeller blade forces is described by an acceleration source. Closed form solutions are presented for the sound field of a propeller in yaw with asymmetric disk loading.

AB - The sound generation due to propeller blade forces is described by an acceleration source. Closed form solutions are presented for the sound field of a propeller in yaw with asymmetric disk loading.

UR - https://www.scopus.com/pages/publications/85040292301

M3 - Article

AN - SCOPUS:85040292301

JO - Mitteilung - Deutsche Forschungs- und Versuchsanstalt fuer Luft- und Raumfahrt

JF - Mitteilung - Deutsche Forschungs- und Versuchsanstalt fuer Luft- und Raumfahrt

ER -

PROPELLERLAERM BEI UNTERSCHALIBLATTSPITZENMACHZAHLEN UMFANGSKRAFT UND AXIALKRAFT. right brace Propeller Noise at Subsonic Blade Tip Speeds, Torque and Thrust Force

Abstract

ASJC Scopus subject areas

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