References

Related Books and Articles

1. Kuechemann,D. The Aerodynamic Design of Aircraft, Pergamon Press, 1978.
   
   
2. Jones,R.T., Wing Theory, Princeton Univ. Press, 1990.
   
   
3. Lock, R., "Aerodynamic Design Methods for Transonic Wings," Aeronautical Journal, January 1990.
   
   
4. Prandtl, L., Tietjens, O., Applied Hydro- and Aeromechanics, McGraw-Hill, 1931, Dover Edition, 1957.
   
   
5. von Karman, T., Burgers, J.M., ``General Aerodynamic Theory -- Perfect Fluids,'' Vol. II of Aerodynamic Theory , W. F. Durand, ed., Dover edition, 1963.
   
   
6. Jones, R., "The Spanwise Distribution of Lift for Minimum Induced Drag of Wings Having Given Lift and Root Bending Moment," NACA TN-2249, 1950.
   
   
7. Cone, C. D. "The Theory of Induced Lift and Minimum Induced Drag of Nonplanar Lifting Systems, NASA TR R-139, 1962.
   
   
8. Blackwell, J., ``Numerical Method To Calculate the Induced Drag or Optimal Span Loading for Arbitrary Non-Planar Aircraft,'' NASA SP-405, May 1976.
   
   
9. Heyson, H. H., Roebe, G. D. and Fulton, C. L. Theoretical Parametric Study of the Relative Advantages of Winglets and Wing-Tip Extensions, NASA TP 1020, 1977.
   
   
10. Munk, M. M. The Minimum Induced Drag of Aerofoils, NACA Report 121, 1921.
    
    
11. Prandtl, Jones, Minimum induced drag with fixed wing weight and constant thickness
    
    
12. Lamar, J., ``A Vortex Lattice Method for the Mean Camber Shapes of Trimmed Non-Coplanar Planforms with Minimum Vortex Drag,'' NASA TN-D-8090, 1976.
    
    
13. Wakayama, S., Kroo, I., "Subsonic Wing Design Using Multidisciplinary Optimization," Proceedings of the 5th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, AIAA-94-4409, Sept. 1994.
    
    
14. Campbell. R., Smith, L., Mineck, R., "Efficient Constrained Aerodynamic Design", NAS Technical Summaries, 1992, NASA Ames Research Center.
    
    
15. Rubbert, P., Tinoco, E., "Impact of Computational Methods on Aircraft Design," AIAA 83-2060, Aug. 1983.
    
    
16. Cosentino, G., Holst,T, "Transonic Wing Design Using Numerical Optimization," J. of Aircraft, 1986.
    
    
17. Jones, R., Lasinski, T., ``Effect of Winglets on the Induced Drag of Ideal Wing Shapes,'' NASA TM 81230, 1980.
    
    
18. Kroo, I., Design and Analysis of Optimally-Loaded Lifting Systems, an updated version of AIAA 84-2507, Oct. 1984.
    
    
19. Kroo, I., McMasters, J., Smith, S.C., Highly Nonplanar Lifting Systems, Presented at: Transportation Beyond 2000: Technologies Needed for Engineering Design NASA Langley Research Center, September 26-28, 1995