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The Kirchhoff Formula for a Supersonically Moving SurfaceThe Kirchhoff formula for radiation from stationary surfaces first appeared in 1882, and it has since found many applications in wave propagation theory. In 1930, Morgans extended the formula to apply to surfaces moving at speeds below the wave propagation speed; we refer to Morgans formula as the subsonic formulation. A modern derivation of Morgans result was published by Farassat and Myers in 1988, and it has now been used extensively in acoustics, particularly for high speed helicopter rotor noise prediction. Under some common conditions in this application, however, the appropriate Kirchhoff surface must be chosen such that portions of it travel at supersonic speed. The available Kirchhoff formula for moving surfaces is not suitable for this situation. In the current paper we derive the Kirchhoff formula applicable to a supersonically moving surface using some results from generalized function theory. The new formula requires knowledge of the same surface data as in the subsonic case. Complications that arise from apparent singularities in the new formulation are discussed briefly in the paper.
Document ID
20040111236
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Farassat, F.
(NASA Langley Research Center Hampton, VA, United States)
Myers, M. K.
(George Washington Univ. Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1996
Subject Category
Acoustics
Report/Patent Number
AIAA Paper 95-062
Report Number: AIAA Paper 95-062
Meeting Information
Meeting: First Joint CEAS/AIAA Aeroacoustics Conference
Location: Munich
Country: Germany
Start Date: June 12, 1995
End Date: June 15, 1995
Sponsors: American Inst. of Aeronautics and Astronautics, National Oceanic and Atmospheric Administration
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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