Planetary Exploration Using Biomimetics An Entomopter <strong>for</strong> Flight on Mars 101.Gault, D. E., “Boundary-Layer and Stalling Characteristics of the NACA 63-009 Airfoil Section,” NACA TN 1894, June 1949. 102.Gibbs-Smith, C. H., “Chapter VI, The First Half of The Nineteenth Century,” A History of Flying, B. T. Bats<strong>for</strong>d, London, 1953, pp. 108-112. 103.Giguere, P., and Selig, M. S., “New Airfoils <strong>for</strong> Small Horizontal Axis Wind Turbines,” ASME Journal of Solar Energy Engineering, Vol. 120, May 1998, pp. 108-114. 104.Gilmour, K.M., Ellington, C.P., Journal of Experimental Biology, No. 183, pg. 101, 1993. 105.Goldstein, S., “On the Vortex Theory of Screw Propellers,” Proceedings of the Royal Society of London, Series A, Vol. 123, 1929, pp. 440-465. 106.Golshan, N., Ho, C., Radiowave Propagation Issues <strong>for</strong> In-Situ Communications, DES- CANSO Symposium, Pasadena, CA, September 21-23, 1999. 107.Gopalarathnam, A., and Selig, M. S., “Low-Speed Natural-Laminar-Flow Airfoils: Case Study in Inverse Airfoil Design,” Journal of Aircraft, Vol. 38, No. 1, Jan.-Feb. 2001, pp. 57- 63. 108.Grasmeyer, J. M. and Keennon, M. T., “Development of the Black Widow Micro Air Vehicle,” Fixed and Flapping Wing Aerodynamics <strong>for</strong> Micro Air Vehicle Applications, T. J. Mueller (Ed.), Prog. in Astronautics and Aeronautics, Vol., 195, 2001. 109.Gridgen Version 13.3, User Manual, Pointwise Inc., 1998, Bed<strong>for</strong>d, Texas. 110.Grodnitsky, D. L. , Form and Function of Insect Wings: The Evolution of Biological Structures, The John Hopkins University Press, 1999. 111. Guglielmo, J. J., and Selig, M. S., “Spanwise Variations in Profile Drag <strong>for</strong> Airfoils at Low Reynolds Numbers,” Journal of Aircraft, Vol. 33, No. 4, July-Aug. 1996, pp. 699-707. 112.Gursul, L, and Ho, C. M., “High Aerodynamic Loads on an Airfoil Submerged in an Unsteady Stream,” AIAA Journal,Vol.30, No.4, 1992, pp. 1117-1120. 113.Hall, K. C., and Hall, S. R., “Minimum Induced Power Requirements <strong>for</strong> Flapping Flight,” Journal of Fluid Mechanics, Vol. 323, Sept. 1996, pp. 285-315. 114.Hall, K. C., Pigott, S. A., and Hall, S. R., “Power Requirements <strong>for</strong> Large-Amplitude Flapping Flight,” Journal of Aircraft, Vol. 35, No. 3, May-June 1998, pp. 352-361. 115.Hall, S. R., “Micro Air Vehicles: Propulsion and Actuation Issues,” Defense Science Study Group V.-Study <strong>Report</strong>s 1996-1997, Volume 1: Papers 1-13, IDA Paper P-3414, <strong>Institute</strong> <strong>for</strong> Defense Analyses, Alexandria, VA, February 1998, pp. 193-206. 116.Hall, S. R., Yang, K. Y., and Hall, K. C., “Helicopter Rotor Lift Distributions <strong>for</strong> Minimum Induced Power Loss,” Journal of Aircraft, Vol. 31, No. 4, 1994, pp. 837-845. 117.Hall, K. C., Pigott, S. A., and Hall, S. R., “Power Requirements <strong>for</strong> Large-Amplitude Flapping Flight,” AIAA Paper 97-0827, Jan. 1997. 118.Hall, K. C. and Hall, S. R., “A Rational Engineering Analysis of the Efficiency of Flapping Flight,” Fixed and Flapping Wing Aerodynamics <strong>for</strong> Micro Air Vehicle Applications, T. J. Mueller (Ed.), Prog. in Astronautics and Aeronautics, Vol., 195, 2001. 119.Handbook of Tables <strong>for</strong> Applied Engineering Science, 2nd Edition CRC press, 1973. Overview of Propulsion Systems <strong>for</strong> a Mars Aircraft 120.Harris, F. D., “Preliminary Study of Radial Flow Effects on Rotor Blades,” Journal of the American Helicopter Society, Vol. 11, No. 3, 1966, pp. 1-21. 121.Heinrich, D. C., “An Experimental Investigation of a Low Frequency Flow Oscillation over a Low Reynolds Number Airfoil near Stall,” M. S. Thesis, Dept. of Aeronautical and Astronautical Engineering, Univ. of Illinois, Urbana, IL, 1994. C-6 <strong>Phase</strong> <strong>II</strong> <strong>Final</strong> <strong>Report</strong>
Appendix C: List of References 122.Hemsch, M. J., and Luckring, J. M., “Connection between Leading-Edge Sweep, Vortex Lift, and Vortex Strength <strong>for</strong> Delta Wings,” Journal of Aircraft, Vol. 7, No. 5, 1990, pp. 473- 475. 123.Ho, C., Golshan, N., Radio Wave Propagation <strong>for</strong> Communication on and around Mars, 23rd NASA propagation experiments Meeting (NAPEX XX<strong>II</strong>I) and ACTS Propagation Studies, Falls Church, VA. June 1999. 124.Hoerner, S. F., and Borst, H. V., Fluid-Dynamic Lift, Hoemer Fluid Dynamics. Brick Town, NJ, 1975. 125.Ikehata, NL, Inoue, T., Ozawa, M., and Matsumoto, S., “Experimental Investigation on Flow Fields of Viscous Fluid around Two-dimensional Wings: Comparison with Computational Results,” Journal of Marine Science and Technology, Vol. 2, 1997, pp. 62-76. 126.Incropera, F.P. and DeWitt, D.P., Fundamentals of Heat and Mass Transfer, John Wiley and Sons 1990. 127.Isaac, K. M., “A New Approach to Calculating Internal Compressible Flows,” Proceedings of the ASME International Computers in Engineering Conference, Boston, Massachusetts, Vol. 3, Bk. No. G0286C, August 1985. 128.Isogai, K., Shinmoto, Y, and Watanabe, Y., “Effects of Dynamic Stall Phenomena on Propulsive Efficiency and Thrust of a Flapping Airfoil,” AIAA Paper 97-1926, June 1997. 129.Johnson, Richard C., Antenna Engineering Handbook, Third Edition, Mc Graw Hill, Inc., New York, 1993, pg. 21-22. 130.Jones, B. M. “An Experimental Study of the Stalling of Wings,” Aeronautical Research Council <strong>Report</strong>s and Memoranda, No. 1588, Dec. 1933, p. 8. 131.Jones, K. D., and Platzer, M. F., “Airfoil Geometry and Flow Compressibility Effects on Wing and Blade Flutter,” AIAA Paper 98-0517, Jan. 1998. 132.Jones, K. D., and Platzer, M. F., “Time-Domain Analysis of Low-Speed Airfoil Flutter,” AIAA Journal, Vol. 34, No. 5, May 1996. 133.Jones, K. D., Lund, T. C. and Platzer, M. F., “Experimental and Computational Investigation of Flapping Wing Propulsion <strong>for</strong> Micro Air Vehicles,” Fixed and Flapping Wing Aerodynamics <strong>for</strong> Micro Air Vehicle Applications, T. J. Mueller (Ed.), Prog. in Astronautics and Aeronautics, Vol., 195, 2001. 134.Jones, R. T., “Wing Flapping with Minimum Energy,” Aeronautical Journal, Vol. 84, July 1980, pp. 214-217. 135.Jones. K. D., Dohring, C. M., and Platzer, M. F., “Experimental and Computational Investigation of the Knoller-Betz Effect,” AIAA Journal, Vol. 36, No. 7, May 1998. 136.Kadlec, R. A., and Davis, S. S., “Visualization of Quasiperiodic Flows” AIAA Journal, Vol. 17, 1979, pp. 1164-1169. 137.Kaplan, D. I. etal, “In-Situ Propellant Production on Mars: The First Flight Demonstration,” 30th Lunar and Planetary Science Conference, March 1999. 138.Kaplan,D.I., Ratliff, J.E., Baird, R.S., Sanders, G.B., Johnson, K.R., Karlmann, P.B., Juanero, K.J.,Baraona, C.R., Landis, G.A., Jenkins, P.P. and Scheiman, D.A., “In-Situ Propellant Production on Mars: The First Flight Demonstration,” 30th Lunar and Planetary Science Conference, Houston Tx. , March 1999. 139.Karlmann, P., Rapp, D., “Sorption Compressor <strong>for</strong> Collecting Atmospheric CO2 on Mars,” JPL New Technology <strong>Report</strong> NPO-20353, NASA Technical Support Package October 1998. C-7
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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 1.2 Origin
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Chapter 1.0 Introduction 1.3 Missio
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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 1.0 Introduction 1.3 Missio
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Chapter 2.0 Entomopter Configuratio
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Chapter 2.0 Entomopter Configuratio
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3. Density: 1.40E-2 kg/m 3 4. Press
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Chapter 3.0 Vehicle Design 3.5 Fuel
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Chapter 3.0 Vehicle Design 3.5 Fuel
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Chapter 4.0 Entomopter Flight Opera
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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 5.0 Potential Payload Funct
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