Flow Modelling
Code | Completion | Credits | Range | Language |
---|---|---|---|---|
2011079 | ZK | 3 | 2P+0C | Czech |
- Course guarantor:
- Martin Luxa
- Lecturer:
- Radka Keslerová, Martin Luxa
- Tutor:
- Radka Keslerová, Martin Luxa
- Supervisor:
- Department of Technical Mathematics
- Synopsis:
-
Fundamental equations of flow, physical similarity, criterion of similarity
Flow in channel, fully-developed turbulent flow
Flow around the bodies, flow separation
Shear flows, laminar and turbulent flows, laminar/turbulent transition
Thin shear layers (boundary layer, free jet, mixing layer, wall flow, wake)
Equatin of motion - simplifications, universal regions
Transonic flow, local supersonic region in flow field
Unsteady propagation of small disturbance in ideal compressible fluid, shock waves theory
Prandt- Meyer flow - solving of supersonic flow fields using the methods of characteristics
Supersonic flow near the leading edge (isolated profile, profile cascade)
Supersonic flow near the trailing edge, preconditions for vortex row formation
Shock waves in interblade channels, theirs interaction with boundary layers
Experimental methods and techniques in high-speed aerodynamics
- Requirements:
- Syllabus of lectures:
-
Fundamental equations of flow, physical similarity, criterion of similarity
Flow in channel, fully-developed turbulent flow
Flow around the bodies, flow separation
Shear flows, laminar and turbulent flows, laminar/turbulent transition
Thin shear layers (boundary layer, free jet, mixing layer, wall flow, wake)
Equatin of motion - simplifications, universal regions
Transonic flow, local supersonic region in flow field
Unsteady propagation of small disturbance in ideal compressible fluid, shock waves theory
Prandt- Meyer flow - solving of supersonic flow fields using the methods of characteristics
Supersonic flow near the leading edge (isolated profile, profile cascade)
Supersonic flow near the trailing edge, preconditions for vortex row formation
Shock waves in interblade channels, theirs interaction with boundary layers
Experimental methods and techniques in high-speed aerodynamics
- Syllabus of tutorials:
- Study Objective:
- Study materials:
-
Schlichting, H., Gersten, K.: Boundary-Layer Theory, Springer, 2016
White, F. M.: Viscous Fluid Flow, 3rd edition, McGraw-Hill, 2006
Dixon, S.L., Hall, C.: Fluid Mechanics, Thermodynamics of Turbomachinery, 6th edition, Elsevier, 2010
Shapiro, A.H.: Compressible Fluid Flow I + II, New York, 1958
Anderson, J.D.: Modern Compressible Flow, New York, 1982
Hirsch, Ch.: Numerical Computation of Internal and External Flows, Butterworth-Heinemann, 2007
Feistauer, M., Felcman, J., Straškraba, I.: Mathematical and Computational Methods for Compressible Flow, Oxford University Press, 2003
- Note:
- Time-table for winter semester 2024/2025:
- Time-table is not available yet
- Time-table for summer semester 2024/2025:
-
06:00–08:0008:00–10:0010:00–12:0012:00–14:0014:00–16:0016:00–18:0018:00–20:0020:00–22:0022:00–24:00
Mon Tue Wed Thu Fri - The course is a part of the following study plans: