Aeroacoustic Data for High Reynolds Number Supersonic Axisymmetric Jets

Aeroacoustic Data for High Reynolds Number Supersonic Axisymmetric Jets PDF Author: John M. Seiner
Publisher:
ISBN:
Category : Air jets
Languages : en
Pages : 124

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Aeroacoustic Data for High Reynolds Number Supersonic Axisymmetric Jets

Aeroacoustic Data for High Reynolds Number Supersonic Axisymmetric Jets PDF Author: John M. Seiner
Publisher:
ISBN:
Category : Air jets
Languages : en
Pages : 124

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Book Description


Aeroacoustic Data for High Reynolds Number Supersonic Axisymmetric Jets

Aeroacoustic Data for High Reynolds Number Supersonic Axisymmetric Jets PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 78

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Aeroacoustic Data for a High Reynolds Number Axisymmetric Subsonic Jet

Aeroacoustic Data for a High Reynolds Number Axisymmetric Subsonic Jet PDF Author: Michael K. Ponton
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 92

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Aeroacoustic Data for High Reynolds Number Supersonic Axisymmetric Jets

Aeroacoustic Data for High Reynolds Number Supersonic Axisymmetric Jets PDF Author: John M. Seiner
Publisher:
ISBN:
Category : Air jets
Languages : en
Pages : 76

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Aeroacoustic Data for a High Reynolds Number Axisymmetric Subsonic Jet

Aeroacoustic Data for a High Reynolds Number Axisymmetric Subsonic Jet PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781726185462
Category :
Languages : en
Pages : 90

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The near field fluctuating pressure and aerodynamic mean flow characteristics of a cold subsonic jet issuing from a contoured convergent nozzle are presented. The data are presented for nozzle exit Mach numbers of 0.30, 0.60, and 0.85 at a constant jet stagnation temperature of 104 F. The fluctuating pressure measurements were acquired via linear and semi-circular microphone arrays and the presented results include plots of narrowband spectra, contour maps, streamwise/azimuthal spatial correlations for zero time delay, and cross-spectra of the azimuthal correlations. A pitot probe was used to characterize the mean flow velocity by assuming the subsonic flow to be pressure-balanced with the ambient field into which it exhausts. Presented are mean flow profiles and the momentum thickness of the free shear layer as a function of streamwise position.Ponton, Michael K. and Ukeiley, Lawrence S. and Lee, Sang W.Langley Research CenterAEROACOUSTICS; CONVERGENT NOZZLES; JET FLOW; SUBSONIC FLOW; HIGH REYNOLDS NUMBER; PRESSURE OSCILLATIONS; FLOW CHARACTERISTICS; ENGINE NOISE; EXHAUST NOZZLES; EXHAUST GASES; MACH NUMBER; PRESSURE MEASUREMENT; PRESSURE DISTRIBUTION; NOISE REDUCTION; FLOW VELOCITY; MOMENTUM; EXHAUST VELOCITY...

Aeroacoustic Data for a High Reynolds Number Axisymmetric Subsonic Jet

Aeroacoustic Data for a High Reynolds Number Axisymmetric Subsonic Jet PDF Author: Michael K. Ponton
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 84

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Aeroacoustics of Flight Vehicles

Aeroacoustics of Flight Vehicles PDF Author: Harvey H. Hubbard
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 616

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NASA Reference Publication

NASA Reference Publication PDF Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 628

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Aeroacoustics of Supersonic Elliptic Jets

Aeroacoustics of Supersonic Elliptic Jets PDF Author: Abbas Khavaran
Publisher:
ISBN:
Category :
Languages : en
Pages : 18

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Supersonic Jet Noise Generated by Large-scale Instabilities

Supersonic Jet Noise Generated by Large-scale Instabilities PDF Author: John M. Seiner
Publisher:
ISBN:
Category : Jet planes
Languages : en
Pages : 52

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