Airframe noise component interaction studies
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Airframe noise component interaction studies

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Published by National Aeronautics and Space Administration, Scientific and Technical Information Office, for sale by the National Technical Information Service in [Washington], Springfield, Va .
Written in English


  • Airframes.,
  • Airplanes -- Noise.

Book details:

Edition Notes

StatementMartin R. Fink and Robert H. Schlinker, United Technologies Research Center.
SeriesNASA contractor report ; NASA CR-3110, NASA contractor report -- NASA CR-3110.
ContributionsSchlinker, Robert H., United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., Langley Research Center., United Technologies Research Center.
The Physical Object
Paginationiv, 134 p. :
Number of Pages134
ID Numbers
Open LibraryOL17648558M

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Aircraft Airframe Noise and Installation Effects- Research Studies Leung CHOI CHOW, Pierre LEMPEREUR, Knut MAU The principal aircraft and engine manufacturers in Europe are facing increasing pressure to reduce aircraft noise by: 1. Almost 40 Years of Airframe Noise Research – What did we achieve? Werner Dobrzynski Airframe noise is generated through the interaction of turbulent Landing Gear Noise – Baseline WT-Studies B 1/16 scale MLG Baseline full scale or close to full scale LG tests. The noise from such aeroplanes during approach is largely dominated by airframe noise, i.e. the noise generated by the interaction of flow and those aircraft components deployed for landing, such as the landing gears and the wing high-lift Werner Dobrzynski, Hanno Heller, Jan Delfs. Aircraft noise pollution is a harmful noise effect produced by any aircraft or its components during the various phases of a flight. Sound production is divided into three categories: Mechanical noise—rotation of the engine parts, most noticeable when fan blades reach supersonic speeds.

Various papers on numerical methods for engine-airframe integration are presented. The individual topics considered include: scientific computing environment for the s, overview of prediction of complex turbulent flows, numerical solutions of the compressible Navier-Stokes equations, elements of. ATAAC – An EU-Project Dedicated to Hybrid RANS/LES Methods. Authors; C.B.: Characterization of unsteady flow structures around tandem cylinders for component interaction studies in airframe noise. AIAA Paper An EU-Project Dedicated to Hybrid RANS/LES Methods. In: Fu S., Haase W., Peng SH., Schwamborn D. (eds) Progress in Hybrid Cited by: Characterization of Unsteady Flow Structures Around Tandem Cylinders for Component Interaction Studies in Airframe Noise. Unsteady Flowfield Around Tandem Cylinders as Prototype for Component Interaction in Airframe Noise. Mehdi Khorrami. AIRFRAME NOISE MODELING APPROPRIATE FOR MULTIDISCIPLINARY DESIGN AND OPTIMIZATION 42nd AIAA Aerospace Sciences Meeting and Exhibit Reno, NV, January 7, uTrailing Edge Noise – Airframe noise component Parametric Noise Metric Studies with NACA and NACA Cited by: