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AERODYNAMICS AND DESIGN FOR ULTRA-L
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I certify that I have read this dis
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Abstract Growing interest in micro-
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Nomenclature A Rotor disk area B Nu
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τ Shear stress ω, Ω Rotor angul
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Contents Acknowledgments...........
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Chapter 5..........................
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List of Tables 3.1 Effect of Airfoi
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List of Figures 2.1 Comparison of I
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5.6 Small test fixture in the large
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6.38 Predicted spanwise thrust dist
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Chapter 1 Introduction 1.1 Looking
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Chapter 1 wind-tunnel facilities an
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1.3 Summary of Contributions Chapte
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Chapter 2 Two-Dimensional Computati
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Chapter 2 The artificial compressib
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Chapter 2 The control volume method
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2.2.4 Comparison with Experiment Th
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Chapter 2 to diverge if significant
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2.4 Flow Field Assumptions The INS2
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Chapter 2 The results of these time
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Chapter 3 Analysis and Design of Ai
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Chapter 3 adverse gradient in the p
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The canonical pressure coefficient
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Chapter 3 reaches α=5.0 and a lift
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Cl 0.50 0.40 0.30 0.20 0.10 0.00 -0
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Re=6000 result due to Reynolds numb
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FIGURE 3.10 NACA 0002 and NACA 0008
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C l C l 0.8 0.7 0.6 0.5 0.4 0.3 0.2
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Chapter 3 The maximum L/D for all n
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3.5 Effect of Leading Edge Shape an
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C l 0.60 0.50 0.40 0.30 0.20 0.10 0
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Chapter 3 prominent droop near the
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Chapter 3 Small improvements in lif
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Chapter 4 Hybrid Method for Rotor D
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Q/r D L Chapter 4 FIGURE 4.1 Typica
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4.2.3 Elimination of Trigonometric
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Chapter 4 applications of interest
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4.2.7 The Distinction Between the A
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Chapter 4 Two input parameters dete
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Chapter 4 simplification, particula
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4.3.3 Conservation of Angular Momen
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Chapter 4 moves downstream is less
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Chapter 4 of the pitch angle at the
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FIGURE 4.6 Converged wake streamlin
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Chapter 4 idealized models. The met
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Chapter 5 Overview of Experimental
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- Page 111 and 112: 5.4.1 Motor Power Supply All tests
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- Page 125 and 126: t/c 0.5 0.4 0.3 0.2 0.1 0.0 FIGURE
- Page 127 and 128: c/R 0.0 0.2 0.4 0.6 0.8 1.0 r/R Cha
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- Page 157 and 158: Thrust per unit span (g) 3.5 3.0 2.
- Page 159 and 160: V total / ωr 1.0 0.9 0.8 Classical
- Page 161 and 162: Torque per unit span (g cm) 0.75 0.
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- Page 167 and 168: Thrust (g) 9 8 7 6 5 4 3 2 38000 40
- Page 169 and 170: x/R 0.4 0.2 0.0 -0.2 Chapter 6 FIGU
- Page 171 and 172: Cl 0.64 0.62 0.60 0.58 0.0 0.2 0.4
- Page 173 and 174: C f 0.125 0.100 0.075 0.050 0.025 0
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- Page 193 and 194: Chapter 8 Conclusions and Recommend
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- Page 201 and 202: References [1] Spedding, G.R., Liss
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[28] Lamb, Sir Horace, Hydrodynamic