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A Study of Supersonic Surface Sources: The Ffowcs Williams-Hawkings Equation and the Kirchhoff FormulaIn this paper we address the mathematical problem of noise generation from high speed moving surfaces. The problem we are solving is the linear wave equation with sources on a moving surface. The Ffowcs Williams-Hawkings (FW-H) equation as well as the govern- ing equation for deriving the Kirchhoff formula for moving surfaces are both this type of partial differential equation. We give a new exact solution of this problem here in closed form which is valid for subsonic and supersonic motion of the surface but it is particularly suitable for supersonically moving surfaces. This new solution is the simplest of all high speed formulations of Langley and is denoted formulation 4 following the tradition of numbering of our major results for the prediction of the noise of rotating blades. We show that for a smooth surface moving at supersonic speed, our solution has only removable singularities. Thus it can be used for numerical work.
Document ID
20040090462
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Farassat, F.
(NASA Langley Research Center Hampton, VA, United States)
Brentner, Kenneth S.
(NASA Langley Research Center Hampton, VA, United States)
Dunn, M. H.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 98-2375
Meeting Information
Meeting: 4th AIAA/CEAS Aeroacoustics Conference
Location: Toulouse
Country: France
Start Date: June 2, 1998
End Date: June 4, 1998
Sponsors: American Inst. of Aeronautics and Astronautics, Confederation of European Aerospace Societies
Distribution Limits
Public
Copyright
Public Use Permitted.
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