On the vortical-flow-prediction capability of an unstructured-grid Euler solver

Evaluation of Stream Flow Prediction Capability of Hydrological Models in the Upper Blue Nile Basin, Ethiopia

Lecture Notes of the Institute for Computer Sciences, Social Informatics and Telecommunications Engineering - Advances of Science and Technology ◽

10.1007/978-3-030-43690-2_14 ◽

2020 ◽

pp. 210-227

Author(s):

Bayu G. Bihonegn ◽

Mamaru A. Moges ◽

Gerawork F. Mulu ◽

Berhanu G. Sinshaw

Keyword(s):

Stream Flow ◽

Hydrological Models ◽

Nile Basin ◽

Blue Nile ◽

Flow Prediction ◽

Blue Nile Basin ◽

Prediction Capability ◽

Upper Blue Nile Basin

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Vortical flow prediction of a diamond wing with rounded leading edges

Aerospace Science and Technology ◽

10.1016/j.ast.2016.02.011 ◽

2016 ◽

Vol 57 ◽

pp. 103-117 ◽

Cited By ~ 8

Author(s):

Mehdi Ghoreyshi ◽

Krzysztof Ryszka ◽

Russell M. Cummings ◽

Andrew J. Lofthouse

Keyword(s):

Vortical Flow ◽

Flow Prediction ◽

Leading Edges

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Daily Stream Flow Prediction Capability of Artificial Neural Networks as influenced by Minimum Air Temperature Data

Biosystems Engineering ◽

10.1016/j.biosystemseng.2006.08.012 ◽

2006 ◽

Vol 95 (4) ◽

pp. 557-567 ◽

Cited By ~ 15

Author(s):

M. Nayebi ◽

D. Khalili ◽

S. Amin ◽

Sh. Zand-Parsa

Keyword(s):

Neural Networks ◽

Artificial Neural Networks ◽

Air Temperature ◽

Stream Flow ◽

Temperature Data ◽

Flow Prediction ◽

Artificial Neural ◽

Prediction Capability ◽

Minimum Air Temperature

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Vortical Flow Prediction of a Moving Aircraft Using Goal-Oriented Anisotropic Mesh Adaptation

23rd AIAA Computational Fluid Dynamics Conference ◽

10.2514/6.2017-3298 ◽

2017 ◽

Author(s):

Eléonore Gauci ◽

Frédéric Alauzet ◽

Alain Dervieux

Keyword(s):

Mesh Adaptation ◽

Vortical Flow ◽

Anisotropic Mesh ◽

Flow Prediction ◽

Anisotropic Mesh Adaptation

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Partitioning and scheduling algorithms and their implementation in FELISA - An unstructured grid euler solver

Parallel Computational Fluid Dynamics 1993 ◽

10.1016/b978-044481999-4/50153-5 ◽

1995 ◽

pp. 225-232

Author(s):

Y.F. Hu ◽

R.J. Blake ◽

J. Peiro ◽

J. Peraire ◽

K. Morgan

Keyword(s):

Unstructured Grid ◽

Scheduling Algorithms ◽

Euler Solver

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Combustor air flow prediction capability comparing several turbulence models

Journal of Propulsion and Power ◽

10.2514/3.23141 ◽

1989 ◽

Vol 5 (2) ◽

pp. 242-248 ◽

Cited By ~ 1

Author(s):

D. L. Rhode ◽

S. T. Stowers

Keyword(s):

Air Flow ◽

Turbulence Models ◽

Flow Prediction ◽

Prediction Capability

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Vortical Flow Prediction of the AVT-183 Diamond Wing

53rd AIAA Aerospace Sciences Meeting ◽

10.2514/6.2015-0292 ◽

2015 ◽

Cited By ~ 3

Author(s):

Mehdi Ghoreyshi ◽

Krzysztof J. Ryszka ◽

Russell M. Cummings ◽

Andrew J. Lofthouse

Keyword(s):

Vortical Flow ◽

Flow Prediction

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Vortical flow prediction for the design of a wind tunnel experiment with a pitching lambda wing

CEAS Aeronautical Journal ◽

10.1007/s13272-014-0120-5 ◽

2014 ◽

Vol 5 (4) ◽

pp. 447-459 ◽

Cited By ~ 5

Author(s):

S. Wiggen ◽

G. Voß

Keyword(s):

Wind Tunnel ◽

Wind Tunnel Experiment ◽

Vortical Flow ◽

Flow Prediction

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APPLICATION OF AN EULER SOLVER TO SELECTED PROBLEMS IN FLIGHT DYNAMICS

Aviation ◽

10.3846/16487788.2007.9635956 ◽

2007 ◽

Vol 11 (2) ◽

pp. 13-22

Author(s):

Janusz Sznajder ◽

Jerzy Zółtak

Keyword(s):

Unsteady Flow ◽

Steady Flow ◽

Vortex Breakdown ◽

Delta Wing ◽

Flow Analysis ◽

Vortical Flow ◽

Flow Equations ◽

Euler Solver ◽

Unsteady Flow Analysis

Several applications of a Euler solver with the formulation of the flow equations in the noninertial reference system with steady and unsteady flow analysis are presented. The steady‐flow applications include determination of aerodynamic derivatives with respect to angular velocity and analysis of vortical flow over a delta wing at high angles of attack with the determination of aerodynamic coefficients and analysis of vortex breakdown. The unsteady flow analysis is applied in the simulation of a rapid manoeuvre for the determination of unsteady forces. The results of this simulation are compared with results of simulations using steady‐flow approximation in order to assess the advantages of unsteady flow analysis in the simulation of aircraft manoeuvres.

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