cfd solver ansys fluent Search Results


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ANSYS inc cfd 3d-steady rans, reynolds stress model (rsm)
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ANSYS inc workbench v20.0
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ANSYS inc fluid dynamics model ansys r14.5
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ANSYS inc cfd software thermal fluid analysis module fluent 2022 r1
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ANSYS inc commercial cfd solver ansys fluent release 2019 r3
Commercial Cfd Solver Ansys Fluent Release 2019 R3, supplied by ANSYS inc, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
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ANSYS inc fluent v. 12.1.4 cfd code
Specifications Table
Fluent V. 12.1.4 Cfd Code, supplied by ANSYS inc, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
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ANSYS inc cfd code fluent v16
Airflow pattern and pressure trend during sedentary breathing cycle ( a ) Magnitude of velocity on the longitudinal plane. In evidence the acceleration across the larynx constriction. ( b ) Static pressure field along the respiratory system at the inspiration peak (t = 1 s). (Fluent <t>v16,</t> <t>CFD-Post</t> v16-Ansys, www.ansys.com ).
Cfd Code Fluent V16, supplied by ANSYS inc, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
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ANSYS inc fluent control-volume cfd package
Airflow pattern and pressure trend during sedentary breathing cycle ( a ) Magnitude of velocity on the longitudinal plane. In evidence the acceleration across the larynx constriction. ( b ) Static pressure field along the respiratory system at the inspiration peak (t = 1 s). (Fluent <t>v16,</t> <t>CFD-Post</t> v16-Ansys, www.ansys.com ).
Fluent Control Volume Cfd Package, supplied by ANSYS inc, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
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fluent control-volume cfd package - by Bioz Stars, 2026-07
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ANSYS inc cfd optimisation 3d quasi-steady rans, rng k-ε & fluent (ansys) av
Airflow pattern and pressure trend during sedentary breathing cycle ( a ) Magnitude of velocity on the longitudinal plane. In evidence the acceleration across the larynx constriction. ( b ) Static pressure field along the respiratory system at the inspiration peak (t = 1 s). (Fluent <t>v16,</t> <t>CFD-Post</t> v16-Ansys, www.ansys.com ).
Cfd Optimisation 3d Quasi Steady Rans, Rng K ε & Fluent (Ansys) Av, supplied by ANSYS inc, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
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Average 90 stars, based on 1 article reviews
cfd optimisation 3d quasi-steady rans, rng k-ε & fluent (ansys) av - by Bioz Stars, 2026-07
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Image Search Results


Specifications Table

Journal: Data in Brief

Article Title: Data from the numerical analysis of radial and tangential leakage of gas in scroll compressors

doi: 10.1016/j.dib.2020.105197

Figure Lengend Snippet: Specifications Table

Article Snippet: Description of data collection , The data for the numerical simulations was collected using ANSYS FLUENT v. 12.1.4 CFD code, which adopts the finite volume method. Several simulations were conducted with different boundary conditions to explore the influence of the dimensionless parameters over the tip and radial leakage in scroll compressors. The data for the developed correlation were collected using a script written in C++..

Techniques: Software

Airflow pattern and pressure trend during sedentary breathing cycle ( a ) Magnitude of velocity on the longitudinal plane. In evidence the acceleration across the larynx constriction. ( b ) Static pressure field along the respiratory system at the inspiration peak (t = 1 s). (Fluent v16, CFD-Post v16-Ansys, www.ansys.com ).

Journal: Scientific Reports

Article Title: Computational fluid dynamic models as tools to predict aerosol distribution in tracheobronchial airways

doi: 10.1038/s41598-020-80241-0

Figure Lengend Snippet: Airflow pattern and pressure trend during sedentary breathing cycle ( a ) Magnitude of velocity on the longitudinal plane. In evidence the acceleration across the larynx constriction. ( b ) Static pressure field along the respiratory system at the inspiration peak (t = 1 s). (Fluent v16, CFD-Post v16-Ansys, www.ansys.com ).

Article Snippet: Numerical simulations were performed with the commercial CFD code Fluent v16 (ANSYS, Inc., Canonsburg, PA, USA) on an Dell T630 Workstation with 64 Gb RAM and two 1.8 GHz CPUs.

Techniques:

Development of the velocity field downstream the trachea at t = 1 s, in terms of velocity magnitude and tangential component of the velocity vectors. In evidence the rotational flow on the plane of proximal trachea, decreasing in the distal section down through the bifurcation. (Fluent v16, CFD-Post v16-Ansys, www.ansys.com ).

Journal: Scientific Reports

Article Title: Computational fluid dynamic models as tools to predict aerosol distribution in tracheobronchial airways

doi: 10.1038/s41598-020-80241-0

Figure Lengend Snippet: Development of the velocity field downstream the trachea at t = 1 s, in terms of velocity magnitude and tangential component of the velocity vectors. In evidence the rotational flow on the plane of proximal trachea, decreasing in the distal section down through the bifurcation. (Fluent v16, CFD-Post v16-Ansys, www.ansys.com ).

Article Snippet: Numerical simulations were performed with the commercial CFD code Fluent v16 (ANSYS, Inc., Canonsburg, PA, USA) on an Dell T630 Workstation with 64 Gb RAM and two 1.8 GHz CPUs.

Techniques:

In evidence the asymmetrical development of the vorticity field at cross section T1, reaching the maximum at the end of the ascendant part of the inhalation cycle (0–1 s). (Fluent v16, CFD-Post v16-Ansys, www.ansys.com ).

Journal: Scientific Reports

Article Title: Computational fluid dynamic models as tools to predict aerosol distribution in tracheobronchial airways

doi: 10.1038/s41598-020-80241-0

Figure Lengend Snippet: In evidence the asymmetrical development of the vorticity field at cross section T1, reaching the maximum at the end of the ascendant part of the inhalation cycle (0–1 s). (Fluent v16, CFD-Post v16-Ansys, www.ansys.com ).

Article Snippet: Numerical simulations were performed with the commercial CFD code Fluent v16 (ANSYS, Inc., Canonsburg, PA, USA) on an Dell T630 Workstation with 64 Gb RAM and two 1.8 GHz CPUs.

Techniques: