Fluid Mechanics and Aerodynamics
Professor Wes Harris
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Fluid Mechanics and Aerodynamics |
| Spring 2002 |
Learning Objectives (.pdf)
Q2F Sample Problems and Solutions Handout
Q4F Sample Problems and Solutions Handout
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Lecture
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Date
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Topic
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Lecture Notes | Anderson, Third Edition |
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F1
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2/6 | Conservation of linear momentum: integral formulation | pp. 112-124 | |
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F2
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2/7 | Conservation of linear momentum: integral formulation |
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F3
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2/8 | Joukowski airfoil; conformal transformations, complex variables | Lecture 3 | [Wes’ notes] |
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F4
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2/11 | Joukowski airfoil; Kutta condition | Lecture 4 | pp. 290-295 |
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F5
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2/13 | Thin Airfoil Theory (TAT) | Lecture 5 | pp. 277-349 |
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F6
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2/13 | TAT |
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F7
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2/19 | TAT | Lecture 7 |
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F8
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2/20 | Wing theory (three dimensional);span, bound vorticity, downwash, wakes | Lecture 8 | pp. 351-417 |
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F9
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2/21 | Lifting line theory; induced angle of attack; induced drag; aspect ratio; elliptic wing loading | Lecture 9 |
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F10
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2/22 | Drag polar; viscous drag; profile drag. Reynolds number | Lecture 10 |
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F11
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2/25 | Summary: Aerodynamics of airfoils, wings and bodies at low speeds | Lecture 11 |
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F12
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2/26 | Review of thermodynamics and the conservation principles | Lecture 12 | pp. 437-463 |
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F13
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2/27 | Wave propagation; acoustics | pp. 465-475 | |
| F14 | 3/1 | Steady, one-dimensional, isentropic flows: area affects, throats, choking. Normal shock waves | Lecture 14 | pp. 475-502 |
| F15 | 3/4 |
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Lecture 15 | pp. 555-586 |
| F16 | 3/5 |
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Lecture 16 |
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| F17 | 3/6 | Two-dimensional compressible flow; oblique shock waves | Lecture 17 | pp.503-532 |
| Q2F | 3/7 | Aerodynamics of airfoils, wings and bodies |
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| F18 | 3/8 | Prandtl-Meyer expansion waves | Lecture 18 | pp. 532-544 |
| F19 | 3/11 | Supersonic thin airfoil theory (STAT) | pp. 544-555 | |
| F20 | 3/12 | STAT |
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| Q4F | 4/4 | Compressible flows:one-dimensional flow, shock waves, airfoils |
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