A Study on Effects of Aircraft Noise Environment on its Structure

Format:

Conference/Event

Author/Creator:

Shijian, Fu, author.

Conference Name:

International Pacific Air and Space Technology Conference and Exposition (1987-11-13 : Melbourne, Australia)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1987

Summary:

In this paper are reported some measurements of the noise environment of the aircraft, discussed the obtained noise load distribution and frequency spectra of the structure, preliminarily analysed the factors affecting the magnitude of parameters concerned and response characteristics of acoustic vibration of the structure, briefly summarized the noise load spectra and the method of drawing up them, the method of acoustic fatigue test and principles for selecting the parameters" through practical example. Some methods and results of analysing and remedying the troubles caused by the acoustic fatigue are also dealt with in the paper

Notes:

Vendor supplied data

Publisher Number:

872450

Access Restriction:

Restricted for use by site license