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Wall-pressure Fluctuations and Pressure-velocity Correlations in a Turbulent Boundary Layer

Wall-pressure Fluctuations and Pressure-velocity Correlations in a Turbulent Boundary Layer
Author: John S. Serafini
Publisher:
Total Pages: 88
Release: 1963
Genre: Fluid dynamics
ISBN:

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This experimental study was carried out at a free-stream Mach number of 0.6 and a Reynolds number per foot of 3.45 x 106. The magnitudes of the wall-pressure fluctuations agree with the Lilley-Hodgson theoretical results. Space-time correlations of the wall-pressure fluctuations generally agree with Willmarth's results for longitudinal separation distances. The convection velocity of the fluctuations is found to increase with increasing separation distances, and its significance is explained. Measurements with the longitudinal component of the velocity fluctuations indicate that the contributions to the wall-pressure fluctuations are from two regions, an inner region near the wall and an outer region linked with the intermittency.


Measurement of Turbulent Boundary Layer Induced Surface Pressure Fluctuations

Measurement of Turbulent Boundary Layer Induced Surface Pressure Fluctuations
Author: Creighton Lane
Publisher:
Total Pages: 0
Release: 2018
Genre:
ISBN:

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The turbulent boundary layer (TBL) noise generated inside an aircraft can have a detrimental impact on humans. In an effort to better understand TBL physics and measurement techniques, measurements of the fluctuating wall-pressure beneath a TBL have been performed in an anechoic wind tunnel. The measurements were made using an array of pressure microphones provided by Bombardier Aerospace. Analysis of frequency spectra indicated several shortcomings of the array, namely a low saturation limit and electrical issues, however the low speed spectra agree well with the Goody prediction model. Furthermore, an investigation of the relationship between wall-pressure and velocity fluctuations was performed using a pinhole mounted microphone and simultaneous hot-wire boundary layer measurements. This revealed flow interference from the hot-wire apparatus, obscuring the expected relationships and trends. Several areas of improvement have been identified, including higher saturation limit microphones, LDA for velocity measurements, and increasing rigidity of the experimental setup.


Numerical Investigation of Pressure Gradient Effect on Wall-pressure Fluctuations

Numerical Investigation of Pressure Gradient Effect on Wall-pressure Fluctuations
Author: Kok Chian Ng
Publisher:
Total Pages: 50
Release: 2013
Genre: Electronic dissertations
ISBN:

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This research investigates the effect of pressure gradient on wall-pressure fluctuations in turbulent boundary layers using a delayed detached eddy simulation (DDES) turbulence scheme. The results are compared to Goody's and Efimtsov's empirical single-point wall-pressure spectrum models. Three different types of pressure gradient conditions were investigated numerically: zero pressure gradient (Flat Plate as a baseline model), favorable pressure gradient (Convex 10, 20, and 40 Plates), and adverse pressure gradient (Concave 10, 20, and 40 Plates). The numerical results were subsequently compared with each other. For the zero pressure gradient case, results compared well with empirical solutions. It was observed that, for cases with adverse pressure gradients, the pressure fluctuations were more chaotic than for the favorable pressure gradient models. In contrast, the favorable pressure gradient models induced lower frequency noise relative to adverse pressure gradient models.


Wall Pressure Fluctuations and Acoustics in Turbulent Pipe Flow

Wall Pressure Fluctuations and Acoustics in Turbulent Pipe Flow
Author: Mark Albert Daniels
Publisher:
Total Pages: 118
Release: 1986
Genre:
ISBN:

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Measurements of the turbulent boundary layer (TBL) wall pressure spectrum and the facility's propagating acoustic field were conducted in the Boundary Layer Research Facility. Subminiature, piezoresistive-type pressure transducers were used. Detailed calibration of the pressure transducers was performed using a standing wave tube. Measured sensitivities of the transducers were within 0.5 dB of factory specifications and measured phase differences between individual transducers were insignificant. The TBL wall pressure spectrum was obtained using a novel signal-processing technique that allowed a minimization of both acoustic and vibration-induced noise. This technique uses pairs of transducer difference signals from an exisymmetric array of three flush-mounted pressure sensors and permits cancellation of the propagating acoustic and vibrationally induced pressure fields. A measurement involving the coherence function between these transducer signals was shown to validate the measured TBL wall pressure spectra and all assumptions used in developing the measurement technique. Non-dimensionalized spectra of the TBL fluctuating wall pressure measured in this investigation are compared to those measured previously. These comparisons substantiated a maximum, normalized transducer diameter for the complete resolution of the high-frequency part of the TBL wall pressure spectrum. In this study, using glycerine as the working fluid, the transducer diameter is less than wall units, a factor of smaller than ever before achieved.


Wall Pressure Fluctuations in a Turbulent Boundary Layer

Wall Pressure Fluctuations in a Turbulent Boundary Layer
Author: William W. Willmarth
Publisher:
Total Pages: 39
Release: 1958
Genre: Turbulent boundary layer
ISBN:

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When a turbulent boundary layer is produced by air flow past a solid surface, the turbulence in the boundary layer can generate a sound field in the free stream and will also induce fluctuating loads on the solid surface. If the surface is flexible, this motion will generate an additional sound field on both sides of the surface. In an initial investigation of the latter form of sound generation, suitable equipment has been developed to measure the fluctuating wall pressure in the turbulent boundary layer. The equipment includes a specially designed low-noise and low-turbulence-level wind tunnel and a small barium titanate transducer and preamplifier combination for frequencies up to 50 kilocycles. The transducer and preamplifier may be useful for other applications. Using this equipment, some of the properties of the wall pressure fluctuations in a turbulent boundary layer have been measured. It was found that the spectrum of the wall pressure fluctuations extended to 50 kilocycles and that the root-mean-square wall pressure was a constant part (0.0035) of the free stream dynamic pressure for 0.2


MEASUREMENT OF TURBULENT BOUNDARY LAYER UNSTEADY WALL PRESSURES BENEATH ELASTOMER LAYERS OF VARIOUS THICKNESSES ON A PLATE.

MEASUREMENT OF TURBULENT BOUNDARY LAYER UNSTEADY WALL PRESSURES BENEATH ELASTOMER LAYERS OF VARIOUS THICKNESSES ON A PLATE.
Author: Cory Smith
Publisher:
Total Pages:
Release: 2019
Genre:
ISBN:

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The attenuation of turbulence induced wall pressure fluctuations through elastomer layers was studied experimentally and analytically. Wall pressure statistics were measured downstream from a backward facing step, with no elastomer present and beneath 2, 3 and 4 mm thick elastomers in a water tunnel facility. The step height, h, was 0.635 cm and the wall pressures were measured at non-dimensional distances of x/h=10, 24, 36 and 54 downstream from the step. The backward facing step was employed to increase the turbulent boundary layer wall pressure spectral levels above those of the water tunnel facility noise. Velocity statistics were measured at locations corresponding to the wall pressure measurements to aid in the interpretation of the wall pressure data. The attenuation of the wall pressure spectra beneath the elastomer layers that was measured experimentally was then compared to analytical model predictions.In the absence of an elastomer layer, the wall pressure spectra, cross-spectra and velocity statistics measured at the various locations downstream from the backward facing step were in excellent agreement with those reported in the archival literature. With the elastomer layers employed at the x/h=10 location, the measured wall pressure spectral levels were the same as those measured in the absence of an elastomer for frequencies at and below the spectral peak. At higher frequencies, the elastomer layers attenuated the wall pressure spectral levels; an effect that increased with increasing elastomer thickness. The streamwise coherence measured beneath the elastomer layers was higher than that measured in the absence of an elastomer layer, an effect which increased with increasing elastomer thickness. It is speculated that this increase in coherence level is due to the ability of the elastomer to support shear stresses, which effectively increases the area over which an eddy influences the stresses measured by the pressure sensors. The high wavenumber filtering of the elastomers was also observed in the coherence at the smallest streamwise separation of /=2.27.An analytical elastomer transfer function, which models the transfer of turbulent boundary layer wall pressures on the surface of an elastomer to the normal stresses through the elastomer, was applied to the turbulent boundary layer wall pressure measurements in the absence of an elastomer layer and compared to measurements beneath the 2, 3, and 4 mm thick elastomer. The attenuation of the turbulent boundary layer wall pressure fluctuations through the elastomer layer using the analytical elastomer transfer function were in excellent agreement with the attenuation measured experimentally through all thicknesses of elastomer and all free stream velocities at which the experiments were performed.


Aerospace America

Aerospace America
Author:
Publisher:
Total Pages: 720
Release: 2001
Genre: Aeronautics
ISBN:

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Author:
Publisher:
Total Pages: 1004
Release: 1976
Genre: Aeronautics
ISBN:

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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.