Relevant bibliographies by topics / Hot flows

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Hot flows'

Author: Grafiati
Published: 4 June 2021
Last updated: 8 February 2022

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Journal articles on the topic "Hot flows"

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Mathews, W. G., and M. Loewenstein. "Hot galactic flows." Astrophysical Journal 306 (July 1986): L7. http://dx.doi.org/10.1086/184693.

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Yuan, Feng, Defu Bu, and Maochun Wu. "Outflow from Hot Accretion Flows." Proceedings of the International Astronomical Union 8, S290 (August 2012): 86–89. http://dx.doi.org/10.1017/s1743921312019278.

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AbstractNumerical simulations of hot accretion flows have shown that the mass accretion rate decreases with decreasing radius. Two models have been proposed to explain this result. In the adiabatic inflow-outflow solution (ADIOS), it is thought to be due to the loss of gas in outflows. In the convection-dominated accretion flow (CDAF) model, it is explained as because that the gas is locked in convective eddies. In this paper we use hydrodynamical (HD) and magnetohydrodynamical (MHD) simulations to investigate which one is physical. We calculate and compare various properties of inflow (gas with an inward velocity) and outflow (gas with an outward velocity). Systematic and significant differences are found. For example, for HD flows, the temperature of outflow is higher than inflow; while for MHD flows, the specific angular momentum of outflow is much higher than inflow. We have also analyzed the convective stability of MHD accretion flow and found that they are stable. These results suggest that systematic inward and outward motion must exist, i.e., the ADIOS model is favored. The different properties of inflow and outflow also suggest that the mechanisms of producing outflow in HD and MHD flows are buoyancy associated with the convection and the centrifugal force associated with the angular momentum transport mediated by the magnetic field, respectively. The latter mechanism is similar to the Blandford & Payne mechanism but no large-scale open magnetic field is required here. Possible observational applications are briefly discussed.
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Loewenstein, Michael, and William G. Mathews. "Evolution of hot galactic flows." Astrophysical Journal 319 (August 1987): 614. http://dx.doi.org/10.1086/165482.

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Ghasemnezhad, Maryam, and Maryam Samadi. "Radial Convection in Hot Accretion Flows." Astrophysical Journal 865, no. 2 (September 26, 2018): 93. http://dx.doi.org/10.3847/1538-4357/aad8af.

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Yan, Cheng. "Hot money in disaggregated capital flows." European Journal of Finance 24, no. 14 (December 13, 2017): 1190–223. http://dx.doi.org/10.1080/1351847x.2017.1411821.

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Bruun, H. H. "Hot-film anemometry in liquid flows." Measurement Science and Technology 7, no. 10 (October 1, 1996): 1301–12. http://dx.doi.org/10.1088/0957-0233/7/10/003.

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Yuan, Feng, Ronald E. Taam, Yongquan Xue, and Wei Cui. "Hot One‐Temperature Accretion Flows Revisited." Astrophysical Journal 636, no. 1 (January 2006): 46–55. http://dx.doi.org/10.1086/497980.

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Renzini, Alvio. "Hot Gas Flows in Elliptical Galaxies." Symposium - International Astronomical Union 171 (1996): 131–38. http://dx.doi.org/10.1017/s0074180900232257.

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Stars in elliptical galaxies lose mass at an overall present rate Ṁ∗ ≃ 1.5 × 10−11LBM⊙yr−1 (e.g., Faber & Gallagher 1976; Renzini & Buzzoni 1986). When allowing for the predicted increase back with cosmological time it turns out that over one Hubble time the stellar population of an elliptical galaxy has cumulatively lost 20-50% of its initial mass, the precise value depending on the IMF. This review focuses on two simple questions: what happens to the gas being lost by the stars? Where is it ultimately disposed?
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Sharma, Prateek, Eliot Quataert, Gregory W. Hammett, and James M. Stone. "Electron Heating in Hot Accretion Flows." Astrophysical Journal 667, no. 2 (October 2007): 714–23. http://dx.doi.org/10.1086/520800.

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Zakamska, Nadia L., Mitchell C. Begelman, and Roger D. Blandford. "Hot Self‐Similar Relativistic Magnetohydrodynamic Flows." Astrophysical Journal 679, no. 2 (June 2008): 990–99. http://dx.doi.org/10.1086/587870.

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Dissertations / Theses on the topic "Hot flows"

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Bardot, Leon. "Explosive volcanism on Santorini : palaeomagnetic estimation of emplacement temperatures of pyroclastics." Thesis, University of Oxford, 1997. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.360162.

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Lazzarini, Lorenzo. "Numerical modeling of a hot-wire anemometer in turbulent flows." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2019. http://amslaurea.unibo.it/17957/.

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The present thesis deals with the numerical modeling of an hot wire anemometer inside a turbulent channel flow at Re_tau=180 with heat transfer. There are two main approaches when studying turbulence: one could follow an experimental path or a numerical approach could be pursued. Experiments showed some issues when measuring turbulence with hot wire anemometry, spatial and temporal filtering are two examples of such problems. In the present work, numerical simulations were performed in order to validate a code that model a hot-wire probe inside a turbulent channel flow. Direct Numerical Simulation (DNS) solved through a spectral code were used to build such model, due to their high level of precision and resolution. A validation process was performed starting from Kim & Moin experience and Kasagi studies related to DNS of channel flow with passive scalar. Following this path we implement inside our code a line source of heat mimicking the hot-wire behaviour. While simulations were running we collected statistics in order to know the values regarding turbulence fluctuations throughout the entire channel. We obtained a new data-set coming from DNS and spectral element method with not only just a passive scalar but a precise implementation of an hot-wire probe.
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Kirk, Daniel Robert 1975. "Aeroacoustic measurement and analysis of transient supersonic hot nozzle flows." Thesis, Massachusetts Institute of Technology, 1999. http://hdl.handle.net/1721.1/29883.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1999.
Includes bibliographical references (p. 195-199).
A transient testing technique for the study of jet noise was investigated and assessed. A shock tunnel facility was utilized to produce short duration, 10-20 millisecond, under expanded supersonic hot air jets from a series of scaled nozzles. The primary purpose of the facility is to investigate noise suppressor nozzle concepts relevant to supersonic civil transport aircraft applications. The shock tube has many strengths; it is mechanically simple, versatile, has low operating costs, and can generate fluid dynamic jet conditions that are comparable to aircraft gas turbine engine exhausts. Further, as a result of shock heating, the total temperature and pressure profiles at the nozzle inlet are uniform, eliminating the noise associated with entropy non-uniformities that are often present in steady state, vitiated air facilities. The primary drawback to transient testing is the brief duration of useful test time. Sufficient time must be allowed for the nozzle flow and free jet to reach a quasi-steady-state before acoustic measurements can be made. However, if this constraint is met, the short run times become advantageous. The test articles are only exposed to the high temperature flow for a fraction of a second, and can be constructed of relatively inexpensive stereo-lithography or cast aluminum. A comparison between shock tunnel transient noise data and steady-state data is presented to ascertain the usefulness of the technique to make acoustic measurements on scaled nozzles. Three types of nozzles are compared in the assessment effort: (1) a series of 0.64 - 1.9 cm exit diameter small-scale round nozzles that can be operated at transient and cold-flow steady-state conditions at the MIT facility for in-house comparison, (2) a series of 5.1 - 10.2 cm exit diameter ASME standard axisymmetric nozzles, and (3) a 1/1 2th scale version of a modern mixer-ejector nozzle. Scaled versions of nozzles (2) and (3) were tested at Boeing's steady-state low speed aeroacoustic facility for comparison to the transient shock tube noise data. The assessment establishes the uncertainty bounds on sound pressure level measurements over the range of frequency bands, nozzle pressure ratios (1.5 - 4.0), total temperature ratios (1.5 - 3.5), and nozzle scales for which the facility can be employed as a substitute and/or as a complimentary mode of investigation to steady-state hot-flow test facilities. Far-field narrowband spectra were obtained at directivity angles from 65 to 145 degrees and the data were extrapolated to full-scale flight conditions consistent with FAR-36 regulations. Nozzle pressure ratio and total temperature ratio were repeatable to within ± 1 percent of desired conditions. The constraint of short test duration is shown to be alleviated through the use of multiple runs to reduce the uncertainty associated with making transient acoustic measurements. Sound pressure level versus frequency trends with nozzle pressure ratio and directivity angle are shown to be comparable between the steady-state and transient noise data for all three nozzle types. The small scale nozzles exhibited agreement to within ± 1 - 2 dB over a full-scale frequency range of 50 - 1250 Hz. The ASME nozzle results demonstrated that the transient noise data replicates the Boeing steady-state data to within 2 - 3 dB on SPL versus full-scale frequency from 250 - 6300 Hz, as well as OASPL and PNL versus directivity angle. The magnitude of EPNL values are shown to agree to within 1 - 3 dB depending on test condition and nozzle scale. The mixer-ejector model exhibited agreement with the steady-state noise data to within 2 - 5 dB over a frequency range of 500 - 6300 Hz for all directivity angles. OASPL and PNL versus directivity angle noise data exhibited agreement with magnitude to within 1 - 4 dB. Steady-state trends with MAR, azimuthal angle, and EPNL were also present in the transient noise data.
by Daniel Robert Kirk.
S.M.
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Laurantzon, Fredrik. "Flow Measuring Techniques in Steady and Pulsating Compressible Flows." Licentiate thesis, KTH, Mekanik, 2010. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-26344.

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This thesis deals with flow measuring techniques applied on steady and pulsatingflows. Specifically, it is focused on gas flows where density changes canbe significant, i.e. compressible flows. In such flows only the mass flow ratehas a significance and not the volume flow rate since the latter depends onthe pressure. The motivation for the present study is found in the use of flowmeters for various purposes in the gas exchange system for internal combustionengines. Applications can be found for instance regarding measurements of airflow to the engine, or measurements of the amount of exhaust gas recirculation.However the scope of thesis is wider than this, since the thesis aims toinvestigate the response of flow meters to pulsating flows. The study is mainlyexperimental, but it also includes an introduction and discussion of several inindustry, common flow measuring techniques.The flow meters were studied using a newly developed flow rig, designedfor measurement of steady and pulsating air flow of mass flow rates and pulsefrequencies typically found in the gas exchange system of cars and smallertrucks. Flow rates are up to about 200 g/s and pulsation frequencies from 0 Hz(i.e. steady flow) up to 80 Hz. The study included the following flow meters:hot-film mass flow meter, venturi flowmeter, Pitot tube, vortex flowmeter andturbine flowmeter. The performance of these meters were evaluated at bothsteady and pulsating conditions. Furthermore, the flow under both steady andpulsating conditions were characterized by means of a resistance-wire basedmass flow meter, with the ability to perform time resolved measurements ofboth the mass flux ρu, and the stagnation temperature T0.Experiments shows that, for certain flow meters, a quasi-steady assumptionis fairly well justified at pulsating flow conditions. This means that thefundamental equations describing the steady flow, for each instant of time,is applicable also in the pulsating flow. In the set-up, back-flow occurred atcertain pulse frequencies, which can result in highly inaccurate output fromcertain flow meters, depending on the measurement principle. For the purposeof finding means to determine when back flow prevails, LDV measurementswere also carried out. These measurements were compared with measurementsusing a vortex flow meter together with a new signal processing technique basedon wavelet analysis. The comparison showed that this technique may have apotential to measure pulsating flow rates accurately.Descriptors: Flow measuring, compressible flow, steady flow, pulsating flow,hot-wire anemometry, cold-wire anemometry.
QC 20101208
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Sigfrids, Timmy. "Hot wire and PIV studies of transonic turbulent wall-bounded flows." Licentiate thesis, KTH, Mechanics, 2003. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-1577.

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The compressible turbulent boundary layer developing over atwo-dimensional bump which leads to a supersonic pocket with aterminating shock wave has been studied. The measurements havebeen made with hot-wire anemometry and Particle ImageVelocimetry (PIV).

A method to calibrate hot-wire probes in compressible ow hasbeen developed which take into account not only the ow velocitybut also the inuence of the Mach number, stagnation temperatureand uid density. The calibration unit consists of a small jetow facility, where the temperature can be varied. The hot wiresare calibrated in the potential core of the free jet. The jetemanates in a container where the static pressure can becontrolled, and thereby the gas density. The calibration methodwas verfied in the at plate zero pressure gradient turbulentboundary layer in front of the bump at three different Machnumbers, namely 0.3, 0.5 and 0.7. The profiles were alsomeasured at different static pressures in order to see theinuence of varying density. Good agreement between the profilesmeasured at different pressures, as well as with the standardlogarithmic profile was obtained.

The PIV measurements of the boundary layer ow in front ofthe 2D bump showed good agreement with the velocity profilesmeasured with hotwire anemometry. The shock wave boundary layerinteraction was investigated for an inlet Mach number of 0.69.A lambda shock wave was seen on the downstream side of thebump. The velocity on both sides of the shock wave as measuredwith the PIV was in good agreement with theory. The shock wavewas found to cause boundary layer separation, which was seen asa rapid growth of the boundary layer thickness downstream theshock. However, no back ow was seen in the PIV-data, probablybecause the seeding did not give enough particles in theseparated region. The PIV data also showed that the shock wavewas oscillating, i.e. it was moving approximately 5 mm back andforth. This distance corresponds to about five boundary layerthicknesses in terms of the boundary layer upstream theshock.

Descriptors:Fluid mechanics, compressible ow,turbulence, boundary layer, hot-wire anemometry, PIV, shockwave boundary layer interaction, shape factor.

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Fiorini, Tommaso. "Hot wire manufacturing and resolution effects in high Reynolds number flows." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2013. http://amslaurea.unibo.it/5217/.

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Lo studio della turbolenza è di fondamentale importanza non solo per la fluidodinamica teorica ma anche perchè viene riscontrata in una moltitudine di problemi di interesse ingegneristico. All'aumentare del numero di Reynolds, le scale caratteristiche tendono a ridurre le loro dimensioni assolute. Nella fluidodinamica sperimentale già da lungo tempo si è affermata l'anemometria a filo caldo, grazie ad ottime caratteristiche di risoluzione spaziale e temporale. Questa tecnica, caratterizzata da un basso costo e da una relativa semplicità, rende possibile la realizzazione di sensori di tipo artigianale, che hanno il vantaggio di poter essere relizzati in dimensioni inferiori. Nonostante l'ottima risoluzione spaziale degli hot-wire, infatti, si può verificare, ad alto numero di Reynolds, che le dimensioni dell'elemento sensibile siano superiori a quelle delle piccole scale. Questo impedisce al sensore di risolvere correttamente le strutture più piccole. Per questa tesi di laurea è stato allestito un laboratorio per la costruzione di sensori a filo caldo con filo di platino. Sono in questo modo stati realizzati diversi sensori dalle dimensioni caratteristiche inferiori a quelle dei sensori disponibili commercialmente. I sensori ottenuti sono quindi stati testati in un getto turbolento, dapprima confrontandone la risposta con un sensore di tipo commerciale, per verificarne il corretto funzionamento. In seguito si sono eseguite misure più specifiche e limitate ad alcune particolari zone all'interno del campo di moto, dove è probabile riscontrare effetti di risoluzione spaziale. Sono stati analizzati gli effetti della dimensione fisica del sensore sui momenti statistici centrali, sugli spettri di velocità e sulle funzioni di densità di probabilità.
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Beirutty, Mohammad Hussein. "Development of a hot-wire measurement technique for moderate intensity three-dimensional flows /." Thesis, Connect to this title online; UW restricted, 1987. http://hdl.handle.net/1773/7074.

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Farrar, B. "Hot-film anemometry in dispersed oil-water flows : Development of a hot-film anemometer based measurement technique for detailed studies of complex two-phase flows and its application.........bubbly water-kerosene and water-air flows." Thesis, University of Bradford, 1988. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.234685.

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Ondore, Faustin Alloise. "An experimental and numerical investigation of turbulent flows in a square duct with 90deg bend." Thesis, Brunel University, 1999. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.286693.

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Lai, Huanxin. "Simulation of two-phase bubbly flows : an inert bubble introduced into a hot liquid." Thesis, Nottingham Trent University, 2003. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.271735.

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Books on the topic "Hot flows"

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Nagabushana, K. A. Heat transfer from cylinders in subsonic slip flows. Hampton, Va: Langley Research Center, 1992.

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Nagabushana, K. A. Heat transfer from cylinders in subsonic slip flows. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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Stainback, P. Calvin. Fluctuation diagrams for hot-wire anemometry in subsonic compressible flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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Logan, P. Uncertainties in hot-wire measurements of compressible turbulent flows implied by comparisons with laser-induced fluorescence. New York: AIAA, 1986.

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Pitts, William M. Response behavior of hot-wires and films to flows of different gases. Gaithersburg, Md: U.S. Dept. of Commerce, National Bureau of Standards, 1985.

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Pitts, William M. Response behavior of hot-wires and films to flows of different gases. Gaithersburg, Md: U.S. Dept. of Commerce, National Bureau of Standards, 1985.

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Pitts, William M. Response behavior of hot-wires and films to flows of different gases. Gaithersburg, Md: U.S. Dept. of Commerce, National Bureau of Standards, 1985.

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Pitts, William M. Response behavior of hot-wires and films to flows of different gases. Gaithersburg, Md: U.S. Dept. of Commerce, National Bureau of Standards, 1985.

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Arab, Rupert Fazal. Statistical analysis of hot-wire calibration coefficients for normal and inclined wires in heated turbulent flows. Ottawa: National Library of Canada, 1995.

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Aichouni, Mohamed. Development and decay of turbulent pipe flows: An experimental and computational study. Salford: Universityof Salford, 1992.

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Book chapters on the topic "Hot flows"

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Manmoto, T. "Radiation from Advection-Dominated Flows." In The Hot Universe, 417–18. Dordrecht: Springer Netherlands, 1998. http://dx.doi.org/10.1007/978-94-011-4970-9_151.

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Renzini, Alvio. "Hot Gas Flows in Elliptical Galaxies." In New Light on Galaxy Evolution, 131–38. Dordrecht: Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-009-0229-9_18.

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Forman, W. "Clusters of Galaxies and Cooling Hot Gas." In Cooling Flows in Clusters and Galaxies, 17–29. Dordrecht: Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-2953-1_2.

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Pellegrini, Silvia. "Hot Gas Flows on Global and Nuclear Galactic Scales." In Hot Interstellar Matter in Elliptical Galaxies, 21–54. New York, NY: Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4614-0580-1_2.

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Messaoudene, Noureddine Ait, and James S. T’ien. "Diffusion Layer Structure in a Thermophoretically Affected Flow Over a Hot Surface." In Instabilities and Turbulence in Engineering Flows, 351–65. Dordrecht: Springer Netherlands, 1993. http://dx.doi.org/10.1007/978-94-011-1743-2_20.

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Massaglia, S. "The Evolution of Non-Spherical Thermal Instabilities in Cooling Flows." In Physical Processes in Hot Cosmic Plasmas, 307–13. Dordrecht: Springer Netherlands, 1990. http://dx.doi.org/10.1007/978-94-009-0545-0_17.

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Debisschop, J. R., S. Sapin, J. Delville, and J. P. Bonnet. "Supersonic Mixing Layer Analysis by Laser Planogram and Hot-Wire Based POD." In Eddy Structure Identification in Free Turbulent Shear Flows, 453–62. Dordrecht: Springer Netherlands, 1993. http://dx.doi.org/10.1007/978-94-011-2098-2_37.

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Bertrand-Corsini, C., C. David, A. Bern, P. Montmitonnet, J. L. Chenot, P. Buessler, and F. Fau. "A Three Dimensional Thermomechanical Analysis of Steady Flows in Hot Forming Processes. Application to Hot Flat Rolling and Hot Shape Rolling." In Modelling of Metal Forming Processes, 271–79. Dordrecht: Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-1411-7_30.

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Knapp, G. R. "Hot and Cold Gas in Early-Type Galaxies: A Comparison of X-Ray, HI and Far Infrared Emission." In Cooling Flows in Clusters and Galaxies, 93–102. Dordrecht: Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-2953-1_10.

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Schumann, Jan-Erik, Markus Fertig, Volker Hannemann, Thino Eggers, and Klaus Hannemann. "Numerical Investigation of Space Launch Vehicle Base Flows with Hot Plumes." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 179–91. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_11.

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Abstract The flow field around generic space launch vehicles with hot exhaust plumes is investigated numerically. Reynolds-Averaged Navier-Stokes (RANS) simulations are thermally coupled to a structure solver to allow determination of heat fluxes into and temperatures in the model structure. The obtained wall temperatures are used to accurately investigate the mechanical and thermal loads using Improved Delayed Detached Eddy Simulations (IDDES) as well as RANS. The investigated configurations feature cases both with cold air and hot hydrogen/ water vapour plumes as well as cold and hot wall temperatures. It is found that the presence of a hot plume increases the size of the recirculation region and changes the pressure distribution on the nozzle structure and thus the loads experienced by the vehicle. The same effect is observed when increasing the wall temperatures. Both RANS and IDDES approaches predict the qualitative changes between the configurations, but the reattachment location predicted by IDDES is up to 7% further upstream than that predicted by RANS. Additionally, the heat flux distribution along the nozzle and base surface is analysed and shows significant discrepancies between RANS and IDDES, especially on the nozzle surface and in the base corner.
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Conference papers on the topic "Hot flows"

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Putra, S. Sandy, C. Hassan, and S. Hariyadi. "Hot pyroclastic deposit as lahar resistor: a case study of Gendol River after the Mt. Merapi 2010 eruption." In DEBRIS FLOWS. Southampton, UK: WIT Press, 2012. http://dx.doi.org/10.2495/deb120091.

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Narayan, Ramesh. "Hot accretion flows—key issues." In Accretion processes in astrophysical systems: Some like it hot! - eigth astrophysics conference. AIP, 1998. http://dx.doi.org/10.1063/1.55890.

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Patinios, Marios, Irvin L. Ong, James A. Scobie, Gary D. Lock, and Carl M. Sangan. "Influence of Leakage Flows on Hot Gas Ingress." In ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/gt2018-75071.

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One of the most important problems facing gas turbine designers today is the ingestion of hot mainstream gases into the wheel-space between the turbine disc (rotor) and its adjacent casing (stator). A rim seal is fitted at the periphery and a superposed sealant flow — typically fed through the bore of the stator — is used to prevent ingress. The majority of research studies investigating ingress do so in the absence of any leakage paths that exist throughout the engine’s architecture. These inevitable pathways are found between the mating interfaces of adjacent pieces of hardware. In an environment where the turbine is subjected to aggressive thermal and centrifugal loading these interface gaps can be difficult to predict and the resulting leakage flows which pass through them even harder to account for. This paper describes experimental results from a research facility which experimentally models hot gas ingestion into the wheel-space of an axial turbine stage. The facility was specifically designed to incorporate leakage flows through the stator disc; leakage flows were introduced axially through the stator shroud or directly underneath the vane carrier ring. Measurements of CO2 gas concentration, static pressure and total pressure were used to examine the wheel-space flow structure with and without ingress from the mainstream gas-path. Data is presented for a simple axial-clearance rim-seal. The results support two distinct flow-structures, which are shown to be dependent on the mass-flow ratio of bore and leakage flows. Once the leakage flow was increased above a certain threshold, the flow structure is shown to transition from a classical Batchelor-type rotor-stator system to a vortex-dominated structure. The existence of a toroidal vortex immediately inboard of the outer rim-seal is shown to encourage ingestion.
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Mielke, Amy, Kristie Elam, and Chih-Jen Sung. "Time-Resolved Rayleigh Scattering Measurements in Hot Gas Flows." In 46th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-262.

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AL-BEIRUTTY, M., S. ARTERBERRY, and F. GESSNER. "A hot-wire measurement technique for complex turbulent flows." In 1st National Fluid Dynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-3600.

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Moodie, T. B., J. P. Pascal, and S. J. D. D’Alessio. "Hot spots and nonhydraulic effects in surface gravity flows." In ADVANCES IN FLUID MECHANICS 2006. Southampton, UK: WIT Press, 2006. http://dx.doi.org/10.2495/afm06018.

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Dillard, Luke N., Mehmed S. Ulcay, and Jay P. Gore. "Effects of Pressure on Minimum Hot Surface Ignition Temperatures (MHSIT) in Hot Air Cross-Flows." In AIAA Scitech 2021 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2021. http://dx.doi.org/10.2514/6.2021-1346.

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Warner, Brian, Patrick A. Woudt, and Magnus Axelsson. "QPOs in CVs: An executive summary." In COOL DISCS, HOT FLOWS: The Varying Faces of Accreting Compact Objects. AIP, 2008. http://dx.doi.org/10.1063/1.3002491.

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Ferreira, Bárbara T., Gordon I. Ogilvie, and Magnus Axelsson. "Excitation of trapped oscillations in discs around black holes." In COOL DISCS, HOT FLOWS: The Varying Faces of Accreting Compact Objects. AIP, 2008. http://dx.doi.org/10.1063/1.3002492.

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Török, Gabriel, and Magnus Axelsson. "3:2?" In COOL DISCS, HOT FLOWS: The Varying Faces of Accreting Compact Objects. AIP, 2008. http://dx.doi.org/10.1063/1.3002493.

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Reports on the topic "Hot flows"

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Pitts, William M., and Bernard J. McCaffrey. Response behavior of hot-wires and films to flows of different gases. Gaithersburg, MD: National Bureau of Standards, 1985. http://dx.doi.org/10.6028/nbs.ir.85-3203.

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Simoneau, J. P., H. Noe, and B. Menant. Large eddy simulation of mixing between hot and cold sodium flows - comparison with experiments. Office of Scientific and Technical Information (OSTI), September 1995. http://dx.doi.org/10.2172/107780.

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Dorney, Daniel J., Roger L. Davis, and David E. Edwards. Investigation of Hot Streak Migration and Film Cooling Effects on Heat Transfer in Rotor/Stator Interacting Flows. Report 1. Fort Belvoir, VA: Defense Technical Information Center, April 1992. http://dx.doi.org/10.21236/ada250688.

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Fabien, Cottier, Gnabéli Roch Yao, Lognon Jean-Louis, and Bütikofer Sarah. How horizontal inequalities lead to conflict in migration countries. Swiss National Science Foundation (SNSF), October 2019. http://dx.doi.org/10.46446/publication_r4d.2019.1.en.

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Structural horizontal inequalities in contexts marked by sustained migration flows contribute to the increased chance of nativist violence. The lack of attention to these two issues has hampered efforts to promote peaceful relations between migrants and natives, as our research in Côte d’Ivoire shows.
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Dayan, M. High performance in low-flow solar domestic hot water systems. Office of Scientific and Technical Information (OSTI), December 1997. http://dx.doi.org/10.2172/578464.

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Keller, Wolfgang. How Trade Patterns and Technology Flows Affect Productivity Growth. Cambridge, MA: National Bureau of Economic Research, March 1999. http://dx.doi.org/10.3386/w6990.

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Trabold, T. A., W. E. Moore, and W. O. Morris. Hot-film anemometer measurements in adiabatic two-phase flow through a vertical duct. Office of Scientific and Technical Information (OSTI), June 1997. http://dx.doi.org/10.2172/350943.

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Bernstein, Shai, Richard Townsend, and Ting Xu. Flight to Safety: How Economic Downturns Affect Talent Flows to Startups. Cambridge, MA: National Bureau of Economic Research, October 2020. http://dx.doi.org/10.3386/w27907.

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Eichengreen, Barry, and Pipat Luengnaruemitchai. Bond Markets as Conduits for Capital Flows: How Does Asia Compare? Cambridge, MA: National Bureau of Economic Research, August 2006. http://dx.doi.org/10.3386/w12408.

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Cerutti, Eugenio, Stijn Claessens, and Andrew Rose. How Important is the Global Financial Cycle? Evidence from Capital Flows. Cambridge, MA: National Bureau of Economic Research, August 2017. http://dx.doi.org/10.3386/w23699.

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