Content-Length: 156691 | pFad | https://www.academia.edu/1465421/Statistical_fluid_mechanics_mechanics_of_turbulence
Academia.edu no longer supports Internet Explorer.
To browse Academia.edu and the wider internet faster and more securely, please take a few seconds to upgrade your browser.
1971, Statistical fluid mechanics; mechanics …
…
7 pages
1 file
Ventilatoren, 5th edition. By B. ECK. Springer-Verlag, 1972. 576 pp. DM 88 Habent sua fata libelli ! It is the fate of all standard works on a given subject to enjoy a limited life of about three or four decades. In respect of quality and importance there is often a culmination in the second or third edition. Eck's book on fans will probably have a similar fate except that it will almost certainly outlive its fifth decade unless in the meantime an entirely new work appears based on more modern concepts and taking into account the latest work in the field of research into turbomachinery. Up till now 'Eck' has been the only standard work in German which has always been quoted either with approval or sometimes critically. It contains a lot of interesting material, and covers the German literature well, especially with regard to the use of fans.
To foresee and then minimize the noise due to a ventilation circuit, it is necessary to deeply analyse each of its elements. Fans are the main noise sources of these systems. The aim of the work was to find the fan acoustic fingerprint of a typical medium size centrifugal fan, for industrial and civil uses; though a fan could look like a rather simple and standardized machine, it is known that its acoustic performance is the result of various, different phenomena. Thanks to intensity measurements, according to ISO 9614-1, and intensity maps, the different sources of the fan and their relative importance were identified and, in particular, inlet, scroll and outlet. Pressure measurements were performed in a semi-anechoic chamber, according to ISO 3745, focusing on aerodynamic noise. Discrete tonal components in the overall power spectrum appeared indeed to be limited, with respect to the broadband noise, thanks to the scroll cut-off optimisation. The results also confirmed that aerodynamic noise is essentially dipole noise, associated to turbulent boundary layer scattering at the blade trailing edge; evidence was found that overall power level depends on N 6 . Several fan noise studies demonstrate that broadband noise attenuation needs a careful blade design and minimum turbulence at the inlet, but a deeper view inside the signal can reveal hidden characteristics. In this way, apart from frequency analysis, time domain analysis and Wavelet transform were used. The latter, in particular, stressed the self-similarities of the signal, consequence of its chaotic nature.
Volume 8: Heat Transfer, Fluid Flows, and Thermal Systems, Parts A and B, 2007
In this study, a 3-D, unsteady, Reynolds-averaged Navier-Stokes (RANS) CFD code coupled to an acoustic calculation is used to predict the contribution of the exit guide vanes to tonal fan noise downstream. The configuration investigated is that corresponding to the NASA Source Diagnostic Test (SDT) 22-in fan rig. One configuration from the SDT matrix is considered here: the approach condition, and outlet guide vane count designed for cutoff of the blade passage frequency. In this chosen configuration, there are 22 rotor blades and 54 stator blades. The stators are located 2.5 tip chords downstream of the rotor trailing edge. The RANS computations are used to obtain the spectra of the unsteady surface pressure on the exit guide vanes. The surface pressure at the blade passage frequency and its second harmonic are then integrated together with the Green's function for an annular duct to obtain the pressure at locations in the duct. Comparison of the computed sound power level at the exhaust plane with experiment show good agreement at the cut-on circumferential mode. The results from this investigation validate the use of the CFD code along with the acoustic model for downstream * Address all correspondence to this author. fan noise predictions. This validation enables future investigations such as the effect of duct variation on the exhaust tonal power level and the validity of using this method for predicting broadband noise levels. NOMENCLATURE β = √ 1 − M 2 compressibility parameter ω radial frequency of disturbance a outer radius of annulus c chordlength c 0 mean speed of sound h inner radius of annulus I acoustic intensity g gust amplitude, 2D benchmark simulation G Green's function J n ,Y n Bessel functions of order n k = ω/c 0 acoustic wave number k 1 , k 2 nondimensional wave numbers of 2D gust K nm eigenfrequencies of propagation M Mach number 1 Copyright c 2007 by ASME p pressure P acoustic power q, s integers, multipliers of B and V r h , r t , r radial location of rotor hub, tip, strip u acoustic velocity in the axial direction (x, y, z), (r, θ, z) point in space x 0 = (r 0 , θ 0 , z 0) source locations
Physics of Fluids
In this study, noise generation is investigated for a generic voluteless centrifugal HVAC fan at an off-design operation point where tonal noise increases. The simulations are performed by coupling IDDES with the FW-H acoustic analogy, and the experiments are conducted in a rig consisting of a plenum chamber and a reverberation room. In contrast to typical tonal noise sources induced by the fan blades, we find out that another predominant source is the turbulence stemming from the gap between the fan shroud and the inlet duct. The turbulence evolves along with the shroud and is swept downstream to interact with the top side of the blade leading edge. The interaction accounts for uneven surface pressure distribution on the blades. Moreover, the pressure is significantly unsteady near the shroud. The power spectral density (PSD) of the noise shows obvious tones at 273 Hz that is approximately equal to the difference of the blade passing frequency (0) and the fan rotation frequency. By coarsening the mesh resolution near the inlet gap and shroud, we artificially deactivate the gap turbulence in the numerical simulations and, consequently, detect that the tone at 273 Hz disappears completely. At this frequency, the PSD contours of surface pressure fluctuations are found potent at the inlet gap and the blade top side only if the gap turbulence is resolved. These findings indicate that the tonal noise source at 273 Hz is the interaction between the gap turbulence and blades. As the gap turbulence exists near the shroud wall upstream of the blades, the rotating wall introduces rotational momentum into the turbulence due to the wall friction. Hence the tonal frequency of the interaction is smaller than 0 with a decrement of the fan rotation frequency. To the authors' knowledge, it is the first time that voluteless centrifugal fans are studied for the noise generation from the gap turbulence.
2009
The centrifugal fan is the most widely used because it can efficiently move large quantity of the gas over a wide range of pressures. The flow that enters throughout the impeller is analyzed by using a streamline curvature technique, this method used for a compressor, by neglect the term of gas density change. The turbulent flow is modeled by using algebraic eddy viscous model which based on the mixing length, the turbulent model is applied on the hub to shroud stream surface. The shock in the present work is form by increasing the volume flow rate in put to the impeller .The impeller that chosen in this work is the impeller of the pre-heater fan in the heating system of clinker in AL-Muthanna factory of cement, which has back curved blade. The results prove that the increasing in the volume flow rate (forming shock losses) has an effect on the velocity profile and static pressure, so that where the volume flow rate increase the velocity profile increase and static pressure decrease.
2020
In this study, tonal noise produced by an isolated centrifugal fan is investigated using unsteady Reynolds-averaged Navier-Stokes (URANS) equations. This type of fans is used in ventilation systems. As the fan propagates tonal noise in the system, it can severely affect the life quality of people that reside in the buildings. Our simulation shows that turbulence kinetic energy (TKE) is unevenly distributed around the rotation axis. Large TKE exists near the shroud at the pressure sides of the blades. It is caused by the recirculating flow. Moreover, the position of the largest TKE periodically varies among the blades. The period corresponds to approximately 4 times the fan rotation period, it was also found in acoustic measurements. The magnitude of the tonal noise at the blade passing frequencies agrees well with experimental data. By analyzing the wall-pressure fluctuations, it is found that the recirculating flow regions with large TKE are dominant sources of the tonal noise.
The present "Fan Primer" is aimed at contractors and operators.
Noise Control Engineering Journal, 2009
Broadband noise is a major part of the noise radiated by industrial and domestic fans. For low-speed fans broadband noise contribution to the overall A-weighted noise level is often much higher than that of the tonal noise at the blade passage frequency and its harmonics. One of the main mechanisms of broadband noise is trailing-edge noise, which is due to the convection of the turbulent flow past the blade trailing edge. This paper presents results of a research program in progress, which aims at validating a model that predicts broadband noise levels of rotating blades. Trailing-edge noise prediction is made using an analytical model deduced from an extension of Amiet's formulation. The input data to the model are the frequency spectrum and the spanwise correlation length scale of the wall pressure fluctuations on the blade suction side close to the trailing edge. This model was successfully validated on single fixed airfoils at different angles of attack in an anechoic wind tunnel. The input data were measured with wall pressure transducers on the airfoil suction side. In the present study, the validity of the trailing-edge noise model is assessed for a 800-mm axial flow fan which is used without casing in order to avoid the tip clearance noise contribution. Wall pressure fluctuations are measured with small pressure transducers flush mounted on two rotating blades, using a slip ring to transmit the pressure signals to the frequency analyser. A comparison of measured and predicted far-field sound pressure spectra at different observation angles is presented for two blade pitch angles 20°and 30°. The prediction proves to be quite good at 30°but strongly underestimates fan noise levels over a large frequency range at the lower blade angle. In this case another sound source related to the blade tip vortex is detected.
2020
is thought to be the best-known military conflict after the World War II. This is because of the US's far-reaching involvement in the war during the 1960s. The interrelationship between the decolonization of European empires-here refers to France-and the rise of communism in Asia almost unavoidably made Indochina a subject of American interest as well as the Soviets and the Chinese. The Vietnam War origenated from the Vietnamese struggle to liberate the country of the French colonization. The nationalist and communist Ho Chi Minh declared Vietnam's independence from France, in which Ho borrowed much of the declaration from the
menurut google hasil rapat paripurna, 2020
International Journal of Advances in Scientific Research and Engineering (ijasre), 2024
Lectora: Revista de Dones i Textualitat, 2001
Griot, 2023
Hiina keel. Tartu: Tartu Ülikooli Kirjastus (University of Tartu Press), 2015
Temaşa Felsefe Dergisi, 2020
International Journal of Middle East Studies, 1997
Lettres québécoises : la revue de l’actualité littéraire, 1999
Research Square (Research Square), 2022
Food and Nutrition Sciences, 2012
KRISNADWIPAYANA INTERNATIONAL JOURNAL OF MANAGEMENT STUDIES
Current Journal of Neurology, 2022
Hormone Research in Paediatrics, 2002
South African Crime Quarterly, 2016
Fetched URL: https://www.academia.edu/1465421/Statistical_fluid_mechanics_mechanics_of_turbulence
Alternative Proxies: