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DEVELOPMENT OF ACOUSTICALLY LINED EJECTOR TECHNOLOGY FOR MULTITUBE JET NOISE SUPPRESSOR NOZZLES BY MODEL AND ENGINE TESTS OVER A WIDE RANGE OF JET PRESSURE RATIOS AND TEMPERATURES

Main Author: NASA, WASHINGTON DC, APRIL 1974
Format: NASA-CR Book
Terbitan: NULL
Online Access: http://kinerja.lib.itb.ac.id/ftmd/index.php/bibliografi/detail/3260
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author NASA, WASHINGTON DC, APRIL 1974
title DEVELOPMENT OF ACOUSTICALLY LINED EJECTOR TECHNOLOGY FOR MULTITUBE JET NOISE SUPPRESSOR NOZZLES BY MODEL AND ENGINE TESTS OVER A WIDE RANGE OF JET PRESSURE RATIOS AND TEMPERATURES
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url http://kinerja.lib.itb.ac.id/ftmd/index.php/bibliografi/detail/3260
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