Planetary Exploration Using Biomimetics An Entomopter <strong>for</strong> Flight on Mars 256.Thomas, G. “Overview of Storage Development DOE Hydrogen Program,” Presentation- US DOE Hydrogen Program 2000 Annual Review, May 2000. 257.Torres, G. E., and Mueller, T. J., “Aerodynamics Characteristics of Low Aspect Ratio Wings at Low Reynolds Numbers,” Fixed and Flapping Wing Aerodynamics <strong>for</strong> Micro Air Vehicle Applications, T. J. Mueller (Ed.), Prog. in Astronautics and Aeronautics, Vol., 195, 2001. 258.Triantafyllou, G. S., Triantafyllou, M. S., and Grosenbaugh, M. A., “Optimal Thrust Development in Oscillating Foils with Application to Fish Propulsion;” Journal of Fluids and Structures, Vol. 7, 1993, pp. 205-224. 259.Tuncer, I.H., Platzer, M. F., and Ekaterinaris, J. A., “Computational Analysis of Flapping Airfoil Aerodynamics,” American Society of Mechanical Engineers Fluids Engineering Division, Summer Meeting, June 1994. 260.Tuncer, I. H., and Platzer, M. F., “Thrust Generation due to Airfoil Flapping,” AIAA Journal, Vol. 34, No. 2, 1996, pp. 324-331. 261.Tuncer, I. H., Lai, J., Ortiz, M. A., and Platzer, M. F., “Unsteady Aerodynamics of Stationary/Flapping Airfoil Combination in Tandem,” AIAA Paper 97-0659, Jan. 1997. 262.Ulaby, F. T., Moore, R., K., Fung, A. K., Microwave Remote Sensing, Active and Passive, Volume <strong>II</strong>. Radar Remote Sensing and Surface Scattering and Emission Theory, Artech House, Inc. Norwood, MA, 1982. 263.Ulander, L. M. H., Ultra-wideband and low-frequency SAR interferometry, IEEE 1996. 264.Ultralife Batteries Inc., Lithium Polymer Specifications, July 2000. 265.van den Berg, C. and Ellington, C.P., “The Vortex Wake of a 'Hovering' Model Hawk Moth,” Phil. Trans. R. Soc. Lond. B, 352, 1997, pp. 317-328. 266.van den Berg, C., and Ellington, C.P., “The Three-Dimensional Leading Edge Vortex of a 'Hovering' Model Hawk Moth,” Philosophical Transactions of the Royal Society B, Vol 352, 1997, pp. 329-340. 267.Van Trees, H. L., Detection, Estimation and Modulation Theory, Vol. 1, Chapter 4, Wiley, NY, 1968. 268.Vest, M. S., and Katz, J., “Unsteady Aerodynamic Model of Flapping Wings,” AIAA Journal, Vol. 34, No. 7, 1996, pp. 1435-1440. 269.Vogel. S., “Flight in Drosophila <strong>II</strong>. Variations in Stroke Parameters and Wing Contour,” Journal of Experimental Biology, Vol. 46, 1967, pp. 383-392. 270.von Karman, T., and Burgers, J. M., “General Aerodynamic Theory-Perfect Fluids,” Aerodynamic Theory, Division E, Vol. <strong>II</strong>, edited by W. F. Durand, Julius Springer, Berlin, 1934, p. 308. 271.von Karman, T., and Burgers, J. M., “Problems of Non-Uni<strong>for</strong>m and Curvilinear Motion,” Aerodynamic Theory, W. F. Durand, Editor-in-Chief, Vol. Il, Division E, Julius Springer, Berlin, 1934, pp. 304-310. 272.Wakeling, J. M., and Ellington, C. P., “Dragonfly Flight I. Gliding Flight and Steady State Aerodynamic Forces,” Journal of Experimental Biology, Vol. 200, 1997, pp. 543-556. 273.Wang, J. “Vortex Shedding and Frequency Selection in Flapping Flight,” Journal of Fluid Mechanics, Vol. 410, 2000, pp. 323-341. 274.Weinig, F., “Lift and Drag of Wings with Small Span,” NACA TM 1151, 1947. 275.Weis-Fogh, T., “Energetics of Hovering Flight in Hummingbirds and in Drosophila,” Journal of Experimental Biology, Vol. 56, 1972, pp. 79-104. C-14 <strong>Phase</strong> <strong>II</strong> <strong>Final</strong> <strong>Report</strong>
Appendix C: List of References 276.Weis-Fogh, T., “Quick Estimates of Flight Fitness in Hovering Animals, Including Novel Mechanisms <strong>for</strong> Lift Production,” Journal of Experimental Biology, Vol. 59, 1973, pp. 169- 230. 277.Weis-Fogh, T., “Unusual Mechanisms <strong>for</strong> the Generation of Lift in Flying Animals,” Scientific American, Vol, 233, No. 5, 1975, pp. 80-87. 278.Wickman, J. H., “In-Situ Mars Rocket and Jet Engines Burning Carbon Dioxide,” AIAA 99-2409, 35th Joint Propulsion Conference, June 1999. 279.Wickman, J. H., “In Situ Martian Rocket and ‘Air Breathing’ Jet Engines”, NASA SBIR <strong>Phase</strong> <strong>II</strong> <strong>Final</strong> <strong>Report</strong>, Contract NAS8-97048, November, 1998 280.Willmott, A.P. and Ellington, C.P., “The Mechanics of Flight in the Hawk Moth Manduca Sexta. I. Kinematics of Hovering and Forward Flight,” J. exp. Biol. 200, 1997, pp. 2705- 2722. 281.Wilmott, A.P., Ellington, C.P., and Thomas, A.L.R., “Flow Visualization and Unsteady Aerodynamics in the Flight of the Hawk Moth Manduca Sexta,” Philosophical Transactions of the Royal Society B, Vol 352, 1997, pp. 303-316. 282.Wilmott, P., “Unsteady Lifting-Line Theory by the Method of Matched Asymptotic Expansions,” Journal of Fluid Mechanics, Vol. 186, Jan. 1988, pp. 303-320. 283.The Wind User's Guide Version 3, User Manual, The NPARC Alliance, July 7, 2000, Cleveland, Ohio. 284.Wong, W., Starkovich, J., Adams, S. and Palaszewski, B., “Cryogenic Gellant and Fuel Formation <strong>for</strong> Metallized Gelled Propellants: Hydrocarbons and Hydrogen with Aluminum”, NASA TM-106698 June 1994. 285.Wonmann, F. X., “Progress in the Design of Low Drag Airfoils,” Boundary Layer and Flow Control, edited by G. V. Lachmann, Pergamon, London, 1961, pp. 748-770. 286.Wooton, R. J., “The Mechanical Design of Insect Wings,” Scientific American, Vol. 263, No. 5, Nov. 1990, pp. 114-120. 287.Wu J. Z., Vakili, A. D., and Wu, J. M., “Review of the Physics of Enhancing Vortex Lift by Unsteady Excitation,” Progress in Aerospace Science, Vol. 28, 1991, pp. 73-131. 288.Wu, T. Y, “Swimming of a Waving Plate,” Journal of Fluid Mechanics, Vol. 10, No. 3, 1961, pp. 321-344. 289.Yuasa, S. and Isoda, H., “Carbon Dioxide Propulsion <strong>for</strong> a Mars Airplane,” AIAA-89-2863, 25th Joint Propulsion Conference,1989. 290.Zaman, K. B. M. Q., McKinzie, D. J., and Rumsey, C. L., “A Natural Low-Frequency Oscillation over Airfoils near Stalling Conditions,” Journal of Fluid Mechanics, Vol. 202, 1989, pp. 403-442. 291.Zhang, Y., Geyer, M. E., Primeggia, C., Transmitter Power Requirements <strong>for</strong> Ultra-Wideband and Wideband Short Pulses in Radar and Communication Applications, NASA Glenn Research Center Contract C-79275-J , <strong>Final</strong> <strong>Report</strong>, March, 2000. 292.Zimmerman, C. H., “Characteristics of Clark Y Airfoils of Small Aspect Ratios,” NACA TR 431, 1932. 293.Zweibel,K. “Thin Films: Past, Present, Future”, National Renewable Energy Laboratory Document, April, 1997. C-15
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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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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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1.3.3.1 Surface Imaging The Entomop
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Chapter 6.0 Media Exposure 6.1 Intr
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Chapter 6.0 Media Exposure 6.6 Spec
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