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

Appendix C: List of References
Appendix C: List of References
1. Abbott, I. H., von Doenhoff, A. E., and Stivers, L. S. Jr., “Summary of Airfoil Data,”
NACA Rept. 824, 1945.
2. Aerospace Operations in Urban Environments, Ch. 6, Enabling Technologies for Urban
Aerospace Operations.
3. Ahmadi, A. R., and Widnall, S. E., “Unsteady Lifting-Line Theory as a Singular Perturbation
Problem, Journal of Fluid Mechanics,” Vol. 153, April 1985, pp. 59-81.
4. Akyurtlu, A. and Akyurtlu, J.F., “Evaluation of On-Board Hydrogen Storage Methods for
High-Speed Aircraft,” NASA-CR-187755, January 1991.
5. Albano, E., and Rodden, W., “A Doublet-Lattice Method for Calculating Lift Distributions
on Oscillating Surfaces in Subsonic Flows,” AIAA Journal, Vol. 7, No. 2, 1969, pp. 279-
285.
6. Allen, D.H., Haisler, W.E., Introduction to Aerospace Structural Analysis, John Wiley &
Sons Publisher 1985.
7. Ames, R., Wong, O. and Komerath, N., “On the Flow Field and Forces Generated by a Flapping
Rectangular Wing 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.
8. Anderson, J. D. J., Fundamentals of Aerodynamics, McGraw-Hill, New York, 1991.
9. Angelo, J.A. and Buden D., “Space Nuclear Power”, Orbit Book Company, 1985.
10. Ashley, H., and Landahl, M., Aerodynamics of Wings and Bodies, Addison-Wesley, Reading,
MA, 1965, pp. 21-50.
11. Augenstein, B.W. (1989), The Mars Airplane Revived-Global Mars Surface Surveys, in:
The Case for Mars III: Strategies for Exploration-Technical, pp. 547-556.
12. Azuma, A., Okamoto, M. and Yasuda, K., “Aerodynamic Characteristics of 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.
13. Azuma, A., Springer-Verlag, The Biokinetics of Flying and Swimming, Tokyo, 1992, pp. 77
- 154.
14. Balow, F. A., “Effect of an Unsteady Laminar Separation Bubble on the Flow Field over an
Airfoil near Stall,” M.S. Thesis, Dept. of Aeronautical and Astronautical Engineering, Univ.
of Illinois. Urbana, IL, 1994.
15. Bartlett, G. E., and Vidal, R. J., “Experimental Investigation of Influence of Edge Shape on
the Aerodynamic Characteristics of Low Aspect Ratio Wings At Low Speeds,” Journal of
the Aeronautical Sciences, Vol. 22, No. 8, 1955, pp. 517-533.
16. Baxter, D. R. J., and East, R. A., “A Survey of Some Fundamental Issues in Micro Air Vehicle
Design,” Proceedings of the CAVs Fourteenth International Conference, Univ. of Bristol,
U.K., 1999, pp. 34.1-34.13.
17. Beer, F.P. and Johnstor, E.R. Jr, Mechanics of Materials, McGraw Hill Publisher, 1981.
18. Beer, F.P. and Johnstor, E.R. Jr, Vector Mechanics for Engineers, McGraw Hill Publisher,
1984.
19. Bents, D. J., Kohout, L. L., McKissock, B. I., Rodriguez, C. D., Withrow, C. A., Colozza,
A. J., Hanlon, J. C. and Schmitz, P. C., “SEI Power Source Alternatives for Rovers and
Other Multi-kWe Distributed Surface Applications”, NASA TM- 104359, September 1991.
C-1