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ESDU 13001:2013

$62.40

The Prediction of Shock Noise from Supersonic Jets Including the Near-Field

Published By Publication Date Number of Pages
ESDU 2013-06 NA
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ESDU 13001 provides a means of estimating shock noise levels in
one-third octave bands emanating from a supersonic jet. The
prediction program accompanying this Item covers both near and far
fields and is applicable to a static nozzle.

The main input parameters that need to be specified are the jet
velocity, static temperature ratio and the diameter of the jet
nozzle.

ESDUpac A1301 can be run to carry out the estimation. ESDUpac
B1301 can be used to facilitate the generation of input files.
MATLAB users can use VIEWpac M1301 to run the program, entering
input data through a graphical user interface. VIEWpac M1301 also
generates a graphical output.

ESDU 13001:2013
$62.40