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izvor podataka: crosbi !

Comparative helicopter noise analysis in static and in-flight conditions (CROSBI ID 543523)

Prilog sa skupa u zborniku | izvorni znanstveni rad | međunarodna recenzija

Novak, Doris ; Bucak, Tino ; Miljković, Dubravko Comparative helicopter noise analysis in static and in-flight conditions // Acoustic'08. Pariz, 2008

Podaci o odgovornosti

Novak, Doris ; Bucak, Tino ; Miljković, Dubravko

engleski

Comparative helicopter noise analysis in static and in-flight conditions

Rotary-wing aircraft is a source of a intense noise, external and internal alike, in conclusion becoming serious environmental and health issue. The generated noise is in some aspects similar to propeller noise in fixed wing aircrafts, while differing in main noise source alignment in respect to the relative airflow: in helicopters, both rotors, i.e. main and tail, that produce force s necessary for flight, and inline with the direction of flight, while the airplane rotor(s) are perpendicular to it. Another distinctive noise in helicopters, well known as 'slapping' comes from the rotor cutting its own wake/wortexs, especially while descending. In this article main helicopter noise sources will be discussed and most significant results of various static and in-flight noise measurement on two different types of helicopter will be presented and analyzed.

helicopter; noise measurement

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Podaci o prilogu

2008.

objavljeno

Podaci o matičnoj publikaciji

Acoustic'08

Pariz:

987-2-9521105-4-9

Podaci o skupu

Acoustic'08

predavanje

29.06.2008-04.07.2008

Pariz, Francuska

Povezanost rada

Elektrotehnika, Tehnologija prometa i transport, Zrakoplovstvo, raketna i svemirska tehnika