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課程名稱 |
可壓縮流體力學
COMPRESSIBLE FLOW |
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開課學期 |
97-2 |
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授課對象 |
工學院 機械工程學研究所 |
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授課教師 |
賴君亮 |
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課號 |
ME7116 |
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課程識別碼 |
522 M2830 |
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班次 |
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學分 |
3 |
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全/半年 |
半年 |
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必/選修 |
選修 |
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上課時間 |
星期三5,6,7(12:20~15:10) |
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上課地點 |
工綜213 |
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備註 |
總人數上限：40人 |
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課程簡介影片 |
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核心能力關聯 |
核心能力與課程規劃關聯圖 |
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課程大綱
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課程概述 |
教導學生明瞭可壓縮流體之特性及流動所呈現的物理現象；教導學生描述與分析可壓縮流場的方法與技巧，期使學生能將所學的知識應用於自然現象的解釋以及相關科技的改進與擴展。 |
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課程目標 |
˙Introduction to Compressible Flow : A Brief Review of Thermodynamics, A Brief Review of Fluid Mechanics, Speed of Sound and Mach Number, Classification of Compressible Flows, Reference State
˙Steady One-Dimensional Compressible Flow : One-Dimensional Flow Equations, Isentropic Flow, Adiabatic Flow in A Constant-Area Duct with Friction, Frictionless Flow in A Constant-Area Duct with Heat Transfer, Normal Shocks, Applications, Combustion Waves : Detonation and Deflagrations
˙Unsteady Wave Motion : Moving Normal Shock Waves, Reflected Shock Wave, One-Dimensional Isentropic Equations, Elements of Acoustic Theory, Isentropic Waves of Finite Amplitude, Centered Expansion Wave, The Shock Tube
˙Oblique Shock and Expansion Waves : Oblique Shock Relations, Shock Polar, Reflections and Interactions, Prandtl-Meyer Expansion Waves, Applications
˙Linearized Flow : The Velocity Potential Equation, The Linearized Velocity Potential Equation, The Linearized Pressure Coefficient, Subsonic Flow Past A Wavy Wall, Similarity Laws for Subsonic Flow, 2-D Supersonic Flow with Small Perturbations, Supersonic Flow Past A Wavy Wall, Supersonic Airfoils
˙Supersonic Flow over Bodies of Revolution : Mathematical Formulation, Axially Symmetric Flow, Conical Flow, General Meridian Shapes, Yawed Body of Revolution in Supersonic Flow
˙Method of Characteristics : Theory of Characteristics, Determination of the Characteristic Lines, Determination of the Compatibility Equation, Numerical Computation, Unit Processes, Theorems about Plane Flow, Computation with Weak, Finite Waves, Design of Supersonic Nozzles, Method of Characteristics for Axisymmetric Irrotational Flow, Method of Characteristics for Rotational Flow
˙ Steady Transonic Flow in Converging-Diverging Nozzles : Determination of the Flow Field in the Throat Region, Determination of the Nozzle Contour of Initial Expansion, Determination of the Initial-Value Line
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課程要求 |
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預期每週課後學習時數 |
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指定閱讀 |
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參考書目 |
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評量方式
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