Selected Topics from High Speed Aerodynamics
Code | Completion | Credits | Range |
---|---|---|---|
W22A004 | ZK | 3P+1C |
- Course guarantor:
- Lecturer:
- Tutor:
- Supervisor:
- Department of Aerospace Engineering
- Synopsis:
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Definition of Compressibility. Fundamentals Principles and Equations of Gas Dynamics for Inviscid, Compressible Flow.
Shock Waves, the Basic Normal Shock Equations.
Oblique Shock Waves and Prandtl-Meyer Expansion Waves.
Measurement of Velocity in a Compressible Flow.
Governing Equations for One-Dimensional Flow.
Adiabatic and Isoentropic Flow in a Variable-Area Streamtube.
Compressible Flow through Nozzles, Diffusers and Wind Tunnels.
Shock-Wave/Viscous Boundary Layer- Interactions.
Subsonic Compressible Flows over Airfoils.
Two-Dimensional supersonic Flows Around Thin Airfoil. Supersonics Airfoils.
Critical Mach Number, Drag-Divergence Mach Number. Supercritical Airfoils.
Transonic Flows over Airfoils.
Swept Wings at Subsonic, Transonic and Supersonic Speeds.
Transonic and Supersonic Flows over Wings and Airplane Configurations.
- Requirements:
- Syllabus of lectures:
-
1.)Definition of Compressibility. Fundamentals Principles and Equations of Gas
Dynamics for Inviscid, Compressible Flow.
2.)Shock Waves, the Basic Normal Shock Equations.
3.)Oblique Shock Waves and Prandtl-Meyer Expansion Waves.
4.)Measurement of Velocity in a Compressible Flow.
5.)Governing Equations for One-Dimensional Flow.
6.)Adiabatic and Isoentropic Flow in a Variable-Area Streamtube.
7.)Compressible Flow through Nozzles, Diffusers and Wind Tunnels.
8.)Shock-Wave/Viscous Boundary Layer- Interactions.
9.)Subsonic Compressible Flows over Airfoils.
10.)Two-Dimensional supersonic Flows Around Thin Airfoil. Supersonics Airfoils.
11.)Critical Mach Number, Drag-Divergence Mach Number. Supercritical Airfoils.
12.)Transonic Flows over Airfoils.
13.)Swept Wings at Subsonic, Transonic and Supersonic Speeds.
14.)Transonic and Supersonic Flows over Wings and Airplane Configurations.
- Syllabus of tutorials:
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Individual Project
- Study Objective:
- Study materials:
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1. Richard S.Shevell
Fundamentals of Flight
2. Barnes W.McCormick
Aerodynamics, aeronautics and Flight Mechanics
3. John D.Anderson,Jr.
Fundamentals of Aerodynamics
4. R.H.Barnard, D.R.Philpott
Aircraft Flight
5. John J.Bertin, Michael L.Smith
Aerodynamics for Engineers
6. Robert W.Fox, Alan T.McDonald
Introduction to Fluid Mechanics
7. Arnold M.Kuethe, Chuen-Yen Chow
Foundation of Aerodynamics
8. James E.A.John
Gas Dynamics
9. John D.Anderson,Jr.
Modern Compressible Flow
- Note:
- Further information:
- No time-table has been prepared for this course
- The course is a part of the following study plans: