A Dynamic Urban Canopy Parameterization for Mesoscale Models Based on Computational Fluid Dynamics Reynolds-Averaged Navier–Stokes Microscale Simulations

2010 ◽  
Vol 137 (3) ◽  
pp. 417-439 ◽  
Author(s):  
J. L. Santiago ◽  
A. Martilli
Author(s):  
Chen Fu ◽  
C Patrick Bounds ◽  
Christian Selent ◽  
Mesbah Uddin

The characterization of a racecar’s aerodynamic behavior at various yaw and pitch configurations has always been an integral part of its on-track performance evaluation in terms of lap time predictions. Although computational fluid dynamics has emerged as the ubiquitous tool in motorsports industry, a clarity is still lacking about the prediction veracity dependence on the choice of turbulence models, which is central to the prediction variability and unreliability for the Reynolds Averaged Navier–Stokes simulations, which is by far the most widely used computational fluid dynamics methodology in this industry. Subsequently, this paper presents a comprehensive assessment of three commonly used eddy viscosity turbulence models, namely, the realizable [Formula: see text] (RKE), Abe–Kondoh–Nagano [Formula: see text], and shear stress transport [Formula: see text], in predicting the aerodynamic characteristics of a full-scale NASCAR Monster Energy Cup racecar under various yaw and pitch configurations, which was never been explored before. The simulations are conducted using the steady Reynolds Averaged Navier–Stokes approach with unstructured trimmer cells. The tested yaw and pitch configurations were chosen in consultation with the race teams such that they reflect true representations of the racecar orientations during cornering, braking, and accelerating scenarios. The study reiterated that the prediction discrepancies between the turbulence models are mainly due to the differences in the predictions of flow recirculation and separation, caused by the individual model’s effectiveness in capturing the evolution of adverse pressure gradient flows, and predicting the onset of separation and subsequent reattachment (if there be any). This paper showed that the prediction discrepancies are linked to the computation of the turbulent eddy viscosity in the separated flow region, and using flow-visualizations identified the areas on the car body which are critical to this analysis. In terms of racecar aerodynamic performance parameter predictions, it can be reasonably argued that, excluding the prediction of the %Front prediction, shear stress transport is the best choice between the three tested models for stock-car type racecar Reynolds Averaged Navier–Stokes computational fluid dynamics simulations as it is the only model that predicted directionally correct changes of all aerodynamic parameters as the racecar is either yawed from the 0° to 3° or pitched from a high splitter-ground clearance to a low one. Furthermore, the magnitude of the shear stress transport predicted delta force coefficients also agreed reasonably well with test results.


1999 ◽  
Vol 43 (04) ◽  
pp. 218-228
Author(s):  
Bin Chen ◽  
Frederick Stern

Computational fluid dynamics results are presented of four-quadrant flow for marine-propulsor P4381. The solution method is unsteady three-dimensional incompressible Reynolds-averaged Navier-Stokes equations in generalized coordinates with the Baldwin-Lomax turbulence model. The method was used previously for the design condition for marine-propulsor P4119, including detailed verification and validation. Only limited verification is performed for P4381. The validation is limited by the availability of four-quadrant performance data and ring vortex visualizations for the crashback conditions. The predicted performance shows close agreement with the data for the forward and backing conditions, whereas for the crashahead and crashback conditions the agreement is only qualitative and requires an ad hoc cavitation correction. Also, the predicted ring vortices for the crashback conditions are in qualitative agreement with the data. Extensive calculations enable detailed description of flow characteristics over a broad range of propulsor four-quadrant operations, including surface pressure and streamlines, velocity distributions, boundary layer and wake, separation, and tip and ring vortices. The overall results suggest promise for Reynolds-averaged Navier-Stokes methods for simulating marine-propulsor flow, including offdesign. However, important outstanding issues include additional verification and validation, time-accurate solutions, and resolution and turbulence modeling for separation and tip and ring vortices.


2020 ◽  
Vol 19 (1-2) ◽  
pp. 95-118 ◽  
Author(s):  
Yuejun Shi ◽  
Seongkyu Lee

This paper uses Reynolds-averaged Navier–Stokes computational fluid dynamics to study trailing edge noise reduction with 3-D finlets. Reynolds-averaged Navier–Stokes computational fluid dynamics provides boundary layer parameters near a trailing edge for an empirical wall pressure spectrum model, and then an acoustic model predicts far-field noise based on pressure fluctuations obtained from the wall pressure spectrum model. First, this numerical approach is validated against experiments. Second, a comprehensive trend analysis is conducted to give insight into the design of 3-D finlets under different flow conditions. A data-driven turbulence spanwise length scale model is developed to tackle finlets with small spacing. Combined with acoustic results, detailed computational flow field results are analyzed to understand the physical mechanism of noise reduction. While the major part of the proposed mechanism is the same as prior work, several new observations are shown which better understand the physical mechanism of noise reduction with 3-D finlets. The goals of the current paper are to provide an efficient Reynolds-averaged Navier–Stokes-based approach to predict trailing edge noise of 3-D finlets, to give complete trend analysis results with various finlets under different flow conditions, and to advance an understanding of the underlying physics.


Author(s):  
J. Johansen ◽  
N. N. So̸rensen ◽  
J. A. Michelsen ◽  
S. Schreck

The Detached-Eddy Simulation model implemented in the computational fluid dynamics code, EllipSys3D, is applied on the flow around the NREL Phase-VI wind turbine blade. Results are presented for flow around a parked blade at fixed angle of attack and a blade pitching along the blade axis. Computed blade characteristics are compared with experimental data from the NREL/NASA Ames Phase-VI unsteady experiment. The Detached-Eddy Simulation model is a method for predicting turbulence in computational fluid dynamics computations, which combines a Reynolds Averaged Navier-Stokes method in the boundary layer with a Large Eddy Simulation in the free shear flow. The present study focuses on static and dynamic stall regions highly relevant for stall regulated wind turbines. Computations do predict force coefficients and pressure distributions fairly good and results using Detached-Eddy Simulation show considerably more three-dimensional flow structures compared to conventional two-equation Reynolds Averaged Navier-Stokes turbulence models, but no particular improvements are seen on the global blade characteristics.


2017 ◽  
Vol 20 (2) ◽  
pp. 181-193 ◽  
Author(s):  
Masumeh Gholamisheeri ◽  
Shawn Givler ◽  
Elisa Toulson

Transient jet ignition of a homogeneous methane air mixture in a turbulent jet ignition system is studied computationally using a large eddy simulation turbulence model. The jet discharges from a prechamber into a main combustion chamber via one or more orifice(s) and provides a distributed ignition source in turbulent jet ignition. The effect of orifice size and stoichiometry is studied numerically using the Converge computational fluid dynamics code. A reduced kinetic mechanism is used for combustion along with a Smagorinsky sub-model for turbulence modeling. The computed pressure traces are compared with experimental measurements through rapid compression machine tests. Computational fluid dynamics results are in acceptable agreement with the experimental data during compression and the early stage of combustion; however, an over-prediction of peak pressure was reported. Peak pressure error is in the range of 0.1%–4% for Reynolds-averaged Navier–Stokes simulation estimation compared to the experimental measurements. This error is a function of mixture stoichiometry and unburned gas temperature. The error calculation showed that with the large eddy simulation model, 1% and 12% improvements in peak pressure and burn rate estimations, respectively, were achieved compared to Reynolds-averaged Navier–Stokes results. The reduced large eddy simulation error relative to the Reynolds-averaged Navier–Stokes simulations were considered to be in the acceptable range; however, further improvements could be achieved through validation and testing of additional turbulence models. In addition, computational fluid dynamics temperature contours for various nozzle orifices and air–fuel ratios are compared to achieve deeper insight into the turbulent jet ignition combustion process in the rapid compression machine combustion cylinder. The numerical iso-surface temperature contours were obtained which enabled three-dimensional views of the flame propagation, the jet discharge, ignition and extinction events. The heat release process and regeneration of mid-range temperature iso-surfaces (1200 K) were not visible through the experimental images.


2015 ◽  
Vol 4 ◽  
pp. 444
Author(s):  
Jorge Maldonado Correa ◽  
Diego Barragán Guerrero

Neste trabalho, apresenta-se o estudo comparativo entre a produção de energia real do parque eólico Villonaco e a produção de energia calculada por Meteodyn WT, que é uma ferramenta CFD (Computational Fluid Dynamics) baseada num modelo de fluxo não lineal e nas equações tridimensionais de Reynolds, Averaged Navier-Stokes. O parque eólico em análise, com uma potência instalada de 16.5 MW, está localizado na província de Loja no sul do Equador, instalado em terreno montanhoso em uma altitude aproximada de 2720 metros sobre o nível do mar, em um setor que opera em condições extremas com velocidade média anual do vento acima de 10.5 m/s e alta complexidade orográfica. Os resultados do modelamento mostram uma produção anual de energia (AEP) do parque eólico Villonaco de 74.8 GWh por ano, um fator de capacidade (CF) de 51% e um total de 4496.2 horas de operação por ano (horas em plena carga), dados que se aproximam da produção real dos registros existentes no parque.


Author(s):  
David Dunham ◽  
Adrian Spencer ◽  
James J. McGuirk ◽  
Mehriar Dianat

It is well documented that various large-scale quasiperiodic flow structures, such as a precessing vortex core (PVC) and multiple vortex helical instabilities, are present in the swirling flows typical of air swirl fuel injectors. Prediction of these phenomena requires time-resolved computational methods. The focus of the present work was to compare the performance and cost implications of two computational fluid dynamics (CFD) methodologies—unsteady Reynolds averaged Navier–Stokes (URANS) using a k-ε model and large eddy simulation (LES) for such flows. The test case was a single stream radial swirler geometry, which has been the subject of extensive experimental investigation. Both approaches captured the gross (time-mean) features of strongly swirling confined flows in reasonable agreement with experiment. The temporal dynamics of the quadruple vortex pattern emanating from within the swirler and observed experimentally were successfully predicted by LES, but not by URANS. Spectral analysis of two flow configurations (with and without a central jet) revealed various coherent frequencies embedded within the broadband turbulent frequency range. LES reproduced these characteristics, in excellent agreement with experimental data, whereas URANS predicted the presence of coherent motions but at incorrect amplitudes and frequencies. For the no-jet case, LES-predicted spectral data indicated the occurrence of a PVC, which was also observed experimentally for this flow condition; the URANS solution failed to reproduce this measured trend. On the evidence of this study, although k-ε based URANS offers considerable computational savings, its inability to capture the temporal characteristics of the flows studied here sufficiently accurately suggests that only LES-based CFD, which captures the stochastic nature of the turbulence much more faithfully, is to be recommended for fuel injector flows.


2014 ◽  
Author(s):  
Νεκτάριος Κουτσουράκης

Στην παρούσα διατριβή έγινε ανάπτυξη υπολογιστικής μεθοδολογίας μοντελοποίησης μεγάλων δινών και χρήση της σε προβλήματα μελέτης της ροής του ανέμου και της διασποράς αέριων ρύπων ανάμεσα σε κτίρια. Η μοντελοποίηση μεγάλων δινών (Large Eddy Simulation – LES) είναι μια μεθοδολογία υπολογιστικής ρευστομηχανικής (Computational Fluid Dynamics – CFD) με την οποία είναι δυνατή η λεπτομερής χρονική επίλυση της ροής και η ανάλυση των μεγάλων δινών της τύρβης. Έτσι η LES ενδείκνυται ιδιαίτερα για μελέτη των ασταθών τυρβωδών ροϊκών φαινομένων που συμβαίνουν σε αστικές γεωμετρίες. Η μεθοδολογία LES που αναπτύχθηκε ενσωματώθηκε σε προϋπάρχοντα κώδικα CFD, τον ADREA-HF. Η αναπτυχθείσα LES χρησιμοποιεί μεταξύ των άλλων και μια πρωτότυπη μέθοδο δημιουργίας τεχνητής ψευδοτύρβης για χρήση σε οριακές συνθήκες του υπολογιστικού χωρίου, η οποία βασίζεται σε μια γενικευμένη εξίσωση τύπου Langevin. Για πιστοποίηση του κώδικα έγιναν μοντελοποιήσεις πλήρως ανεπτυγμένης ροής σε κανάλι, αλλά και ροής και διασποράς ρύπων σε οδικές χαράδρες. Επίσης εξετάστηκαν και πιο σύνθετες περιπτώσεις, όπως έκλυση και διασπορά υδρογόνου σε κλειστούς χώρους, ροή και διασπορά ρύπων σε ασύμμετρες οδικές χαράδρες, ροή πάνω από πολύ μεγάλη τραχύτητα εδάφους και τέλος ροή και διασπορά ρύπων σε μια πρωτότυπη γεωμετρία ημι-εξιδανικευμένης πόλης. Στις εφαρμογές που μελετήθηκαν έγινε επιτυχής σύγκριση με πειραματικά δεδομένα, οπότε η μεθοδολογία που αναπτύχθηκε αποδείχθηκε αξιόπιστη. Εκτός από την LES, χρησιμοποιήθηκε και η απλούστερη μεθοδολογία RANS (Reynolds-Averaged Navier-Stokes), προσδιορίστηκε ο σχετικός ρόλος των δύο μεθοδολογιών και αναδείχθηκαν οι δυνατότητες συμπληρωματικής χρήσης τους στο ίδιο πρόβλημα. Σε κάθε πρακτική εφαρμογή που εξετάστηκε, μελετήθηκαν κυρίως θέματα στα οποία υπήρχε κενό στη βιβλιογραφία. Μεταξύ άλλων προσδιορίστηκαν οι μηχανισμοί απαγωγής των ρύπων σε ασύμμετρες οδικές χαράδρες και υπολογίστηκε για πρώτη φορά ο κρίσιμος λόγος υψών για δημιουργία δύο στροβίλων σε χαράδρες μείωσης αναβαθμού. Επίσης μελετήθηκαν λεπτομερώς ασταθή ροϊκά φαινόμενα και τυρβώδεις δομές στην ημι-εξιδανικευμένη πόλη, αποκαλύπτοντας φαινόμενα όπως ριπές ανέμου, εξωθήσεις ρύπου, μη-γκαουσιανές κατανομές ταχυτήτων, αλλά και μηχανισμούς δημιουργίας κάποιων συνεκτικών δομών της τύρβης (ιδίως πεταλοειδών στροβίλων). Με τη μεθοδολογία LES, ανοίγονται νέοι ορίζοντες στη μελέτη της τυρβώδους ροής και της διασποράς ρύπων στο αστικό περιβάλλον.


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