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A closed-form solution for noise contoursAn analytical approach for generating noise contours that overcome the difficulties of existing programs is described. This approach is valid for arbitrarily complex paths and reveals the importance of various factors that influence contour shape and size. The calculations are simple enough to be implemented on a small, hand-held programmable calculator, and a program for the HP-67 calculator is illustrated. The method is fast, simple, and gives the area, the contour, and its extremities for arbitrary flight paths for both takeoffs and landings.
Document ID
19800003620
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Stewart, E. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Carson, T. M.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1979
Subject Category
Acoustics
Report/Patent Number
A-7660
NASA-TP-1432
Report Number: A-7660
Report Number: NASA-TP-1432
Accession Number
80N11869
Funding Number(s)
PROJECT: RTOP 505-07-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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