LANDING GEAR AND CAVITY NOISE PREDICTION
Prediction of airframe noise radiation from the landing gear and wheel wells of commercial aircraft is examined. Measurements of these components on typical aircraft are presented and potential noise sources identified. Semiempirical expressions for the sound generation by these sources are developed from available experimental data and theoretical analyses. These expressions are employed to estimate the noise radiation from the landing gear and wheel wells for a typical aircraft and to rank order the component sources. (Author)
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Corporate Authors:
Bolt, Beranek and Newman, Incorporated
50 Moulton Street
Cambridge, MA United States 02138 -
Authors:
- Bliss, D B
- Hayden, R E
- Publication Date: 1976-7
Media Info
- Pagination: 57 p.
Subject/Index Terms
- TRT Terms: Acoustic generators; Aircraft; Aircraft noise; Airframes; Civil aircraft; Jet propelled aircraft; Landing gear; Mathematical prediction; Noise; Parts; Vibration; Wheels
- Uncontrolled Terms: Aircraft parts
- Old TRIS Terms: Sound generators
- Subject Areas: Aviation; Data and Information Technology; Environment; Vehicles and Equipment;
Filing Info
- Accession Number: 00145777
- Record Type: Publication
- Source Agency: National Technical Information Service
- Report/Paper Numbers: NASA-CR-2714
- Contract Numbers: NASA ORDER L-18051-A
- Files: TRIS
- Created Date: Jan 16 1977 12:00AM