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

Appendix C: List of References
160.Lighthill, M. J., “Some Challenging New Applications for Basic Mathematical Methods in
the Mechanics of Fluids That Were Originally Pursued with Aeronautical Aims,” Aeronautical
Journal, Vol. 94, No. 932, Feb. 1990, pp. 41-52.
161.Lippisch, A. M., “Man Powered Flight in 1929,” Journal of the Royal Aeronautical Society,
Vol. 64, July 1960, pp. 395-398.
162.Liu, H., and Kawachi, K., “A Numerical Study of Insect Flight,” Journal of Computational
Physics, Vol. 146, 1998, pp. 1-33.
163.Liu, H. and Kawachi, K., “Leading Edge Vortices of Flapping and Rotary Wings at Low
Reynolds Number,” Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications,
T. J. Mueller (Ed.), Prog. in Astronautics and Aeronautics, Vol., 195, 2001.
164.Liu, P., “A Time-Domain Panel Method for Oscillating Propulsors with Both Chordwise
and Spanwise Flexibility,” Ph.D. Thesis, Univ. of Newfoundland, St. John's, NF, Canada,
1996.
165.Liu, P., “Three-Dimensional Oscillating Foil Propulsion,” M.S. Engineering Thesis, Univ.
of Newfoundland, St. John's, NF, Canada, March 1991.
166.Liu. H., Ellington, C.P., Kawachi, K., van den Berg, C. and Willmott, A.P., “A Computational
Fluid Dynamic Study of Hawk Moth Hovering,” J. exp. Biol. 201, 1998, pp. 461-477.
167.Lowry, J. G., and Polhamus, E. C., “A Method for Predicting Lift Increments due to Flap
Deflection at Low Angles of Attack in Incompressible Flow,” NACA TN 3911, 1957.
168.Lowson, M. V., “Aerodynamics of Airfoils at Low Reynolds Numbers,” Proceedings of the
UAVs Fourteenth International Conference, Univ. of Bristol, U.K., 1999, pp. 35.1-35.16.
169.Lund, T. C., “A Computational and Experimental Investigation of Flapping Wing Propulsion,”
M.S. Thesis, Dept. of Aeronautics and Astronautics, Naval Postgraduate School,
Monterey. CA, March 2000.
170.Lunia, A., Isaac, K. M., Chandrashekhara, K., and Watkins, S., “Wind Tunnel Testing of a
Smart Composite Wing using Fiber Optic Strain Sensing and Neural Network,” Smart
Materials and Structures, 9, (2000), 767-773.
171.Lyon, C. A., Broeren, A. P., Gigure, P., Gopalarathnam, A., and Selig, M. S., Summary of
Low-Speed Airfoil Data, Vol. 3, SoarTech Publications, Virginia Beach, VA, 1998.
172.Lyon, C. A., Selig, M. S., and Broeren, A. P., “Boundary Layer Trips on Airfoils at Low
Reynolds Numbers,” AIAA Paper 97-0511, Jan. 1997.
173.Mabey, D. G., “Analysis and Correlation of Data on Pressure Fluctuations in Separated
Flow,” Journal of Aircraft, Vol. 9, No. 9, Sept. 1972, pp. 642-645.
174.Mahafza, B. R., Radar Systems Analysis and Design Using Matlab, Chapman and Hall/
CRC, New York, 2001.
175.Mars Expedition Strategy Group, NASA, “The Search for Evidence of Life on Mars,” JPL,
1996.
176.Maxworthy, T., “Experiments on the Weis-Fogh Mechanism of Lift Generation by Insects
in Hovering Flight. Part 1. Dynamics of the `Fling',” Journal of Fluid Mechanics, Vol. 93,
1979, pp. 47-63.
177.McClaine, A.W., Breault,R.W., Larsen,C., Konduri,R., Rolfe,J. and Becker,F., “Advanced
Chemical Hydride Hydrogen-Generation/Storage System for PEM Fuel Cell Vehicles,”
Thermo Technologies, DOE 2000 Progress Report Contract No. 98111.
178.McCullough, G. B., and Gault, D. E., “Boundary-Layer and Stalling Characteristics of the
NACA 64A006 Airfoil Section,” NACA TN 1923, Aug. 1949.
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