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Aerodynamics II

The course is not on the list Without time-table
Code Completion Credits Range Language
2221232 Z,ZK 4 2P+2C Czech
Garant předmětu:
Department of Aerospace Engineering

The course is focused on the compressible gas dynamics (principially air) and its applications in aerospace. Main topics are gas dynamics, subsonic, transsonic ans supersonic flow round airfoil and wing, shock waves and their formation and characteristics (normal, obligue and lambda waves).


Aerodynamics I

Syllabus of lectures:

1.Compressibility of gas. Basic properties of subsonic, transsonic and supersonic flow. Stlačitelnost plynů. Charakter subsonického, transsonického a supersonického obtékání těles. Propagation of sound waves.

2.Basic laws for compressible flow. Basics of gas dynamics. Aerodynamic heating. Measurement of velocity and state properties in compressible flow.

3.1D compressible flow, adiabatic, with friction, with heat transfer.

4.Flow in nozzles and diffusers. Shock wave formation, obligue shock wave.

5.Planar potential compressible flow.

6.Viscous compressible flow.

7.Subsonic flow on airfoil. Critical Mach number. Aerodynamic coefficiens.

8.Subsonic flow on straight and swept wings.

9.2D supersonic flow. Convex and concave edge flow.

10.Supersonic airfoils.

11.Supersonic flow and wing aerodynamics.

12.Transsonic phenomena.

13.Hypersonic flow.

Syllabus of tutorials:

1.Prandtl equation and its solution, Glauert?s method.

2.Derivation and use of equations for compressible flow. Dependence of Mach number and velocity parameter. Expression of dimensionless state variables.

3.Compressibility of gases. Pressure disturbance propagation. Aerodynamic heating.

4.Graphical formulation of the Bernoulli integral and critical values of dimensionless variables.

5.Adiabatic, isoentropic flow in a tube of variable cross-section.

6.Compressible fluid flow through nozzles, diffusers and wind tunnel.

7.Shock waves.

8.Pressure conditions in the high speed measurement probes.

9.Speed ratios at incompressible and compressible flow on the profile.

10.Aerodynamic characteristics of a profile in subsonic compressible flow.

11.Critical Mach number.

12.Supersonic flow around convex and concave shapes.

13.Two-dimensional supersonic flow around an aerodynamic profile. Supersonic profiles.

Study Objective:

The aim of the course is to deepen the knowledge at the field of aerodynamics by cases of flow around the wing and cases of compressible subsonic, transonic and supersonic flow. Course participants will become familiar with both, the external flow and the flow in channels and nozzles.

Study materials:

•Anderson, J., Modern Compressible Flow: With Historical Perspective, 4th edition, McGraw-Hill, 2021, ISBN 9781260471441

•Anderson, J., Fundamentals of Aerodynamics, 6th edition, McGraw-Hill, 2017, ISBN 9781259129919

•Shapiro, A. H., The Dynamics and Thermodynamics of Compressible Fluid Flow, Wiley, 1977, ISBN: 978-0-471-06691-0

Further information:
No time-table has been prepared for this course
The course is a part of the following study plans:
Data valid to 2024-04-16
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