Phase II Final Report - NASA's Institute for Advanced Concepts

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Planetary Exploration Using Biomimetics An Entomopter for Flight on Mars Figure 3-74: Lift Convergence History. U=14 m/s. α = 34.8 o . Figure 3-75: Drag Convergence History. U=14 m/s. α = 34.8 o . 94 Phase II Final Report
Chapter 3.0 Vehicle Design 3.3 Wing Aerodynamics 3.3.1.4.2 Additional Three-dimensional Cases 3.3.1.4.2.1 Entomopter Wing (Current Design) Next a preliminary 3D simulation was run with heaving. The top and side views of the wing are shown in Figures 3-76 and 3-77, respectively. Figure 3-76: Top View of Entomopter Wing Figure 3-77: Side View of Entomopter Wing The conditions used to run the case were the same as those for the 2D cases given in Table 3-5. The oscillating conditions used were: maximum velocity = 10 m/s, frequency = 20 rad/s. This case was with the wing heaving up and down. The lift and drag coefficients obtained for the heaving case are shown in Figures 3-78 and 3-79. 95
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Planetary Exploration Using Biomime
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Table of Contents Table of Contents
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List of Tables List of Tables Table
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List of Figures List of Figures Fig
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List of Figures Figure 3-54: Pressu
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List of Figures Figure 3-138: Stere
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List of Figures Figure 4-24: Averag
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List of Contributors List of Contri
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Executive Summary Executive Summary
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Chapter 1.0 Introduction Chapter 1.
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Chapter 1.0 Introduction Figure 1-2
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Chapter 1.0 Introduction 1.1 Histor
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Chapter 1.0 Introduction 1.2 Origin
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Chapter 1.0 Introduction 1.3 Missio
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1.3.3.1 Surface Imaging The Entomop
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Chapter 2.0 Entomopter Configuratio
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Chapter 3.0 Vehicle Design 3.1 Wing
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Chapter 3.0 Vehicle Design 3.4 Reci
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Chapter 3.0 Vehicle Design 3.5 Fuel
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Chapter 3.0 Vehicle Design 3.6 Powe
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Chapter 4.0 Entomopter Flight Opera
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Chapter 5.0 Potential Payload Funct
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Chapter 6.0 Media Exposure 6.1 Intr
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Chapter 6.0 Media Exposure 6.3 Onli
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Chapter 6.0 Media Exposure 6.6 Spec
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Chapter 7.0 Conclusion Chapter 7.0
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Appendix A: Mars Atmosphere Data JP
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Appendix A: Mars Atmosphere Data Ge
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Appendix A: Mars Atmosphere Data Ge
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Appendix A: Mars Atmosphere Data Ma
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Appendix B: Sizing Results Appendix
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Appendix B: Sizing Results 30 Wing
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Appendix B: Sizing Results 16 Wing
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Appendix B: Sizing Results Length 0
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Appendix B: Sizing Results Lenght 0
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Appendix C: List of References Appe
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Appendix C: List of References 41.
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Phase II Final Report - NASA's Institute for Advanced Concepts

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