NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Acoustic tests of a 15.2 centimeter-diameter potential flow convergent nozzleAn experimental investigation of the jet noise radiated to the far field from a 15.2-cm-diam potential flow convergent nozzle has been conducted. Tests were made with unheated airflow over a range of subsonic nozzle exhaust velocities from 62 to 310m/sec. Mean and turbulent velocity measurements in the flow field of the nozzle exhaust indicated no apparent flow anomalies. Acoustic measurements yielded data uncontaminated by internal and/or background noise to velocities as low as 152m/sec. Finally, no significantly different acoustic characteristics between the potential flow nozzle and simple convergent nozzles were found.
Document ID
19740019374
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Karchmer, A. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Dorsch, R. G.
(NASA Lewis Research Center Cleveland, OH, United States)
Friedman, R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1974
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-2980
Report Number: NASA-TM-X-2980
Accession Number
74N27487
Funding Number(s)
PROJECT: RTOP 501-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available