References for the Doublet Lattice Program

The first item is the primary reference for this program.

  1. Blair, Max: A Compilation of the Mathematics Leading to the Doublet Lattice Method. USAF Wright Laboratory Report WL-TR-92-3028 (AD-A256 304), March 1992.
  2. Edward Albano and William P. Rodden, "A Doublet Lattice Method for Calculating Lift Distributions on Oscillating Surfaces in Subsonic Flows", AIAA Journal, Vol. 7, No. 2, p 279-285, February 1969
  3. L. V. Andrews and H. T. Vivian, "Unsteady Aerodynamics for Advanced Configurations, Part I - Application of the Subsonic Kernal Function to Nonplanar Lifting Surfaces", FDL-TDR-64-152, May 1965., (Also credited: Dr. E. R. Rodenich).
  4. Raymond L. Bisplinghoff, Holt Ashley, Robert L. Halfman, "Aeroelasticity", Addison Wesley Publishing Co., 1955.
  5. David L. Colton, "Partial Differential Equations, an Introduction", Random House 1988.
  6. Earl H. Dowell, Howard C. Curtiss, Jr., Robert H. Scunlan, "A Modern Course in Aeroelasticity", ijthoff and Noordhoff, Alphen aan den Rijn, The Netherlands, 1978.
  7. I. E. Garrick-, "Nonsteady Wing Characteristics", Section F of the text, "Aerodynamic Components of Aircraft at High Speeds", Vol VII of the series, "High Speed Aerodynamics and Jet Propulsion", editors , X.X. Donovan and H. R. Lawrence. Princeton University Press 1957.
  8. Giesing, J.P., Kalman T.P., Rodden W.P.: Subsonic Unsteady Aerodynamics for General Configurations, Part I - Vol I - Direct Application of the Nonplanar Doublet Method. AFFDL-TR-71-5, November 1971.
  9. Guderley, Karl G. The Initial Stage of Wake Development in Linearized Incompressible and Compressible Flows, AFWAL-TR-86-3120, March 1987.
  10. Rodden, J. P. Giesing, "Application of the Doublet Lattice Method to Nonplanar Configurations in Subsonic Flow", AIAA Journal of Aircraft, Vol. 8, No. 6, p 406-413, June 1971.
  11. Francis B. Hildebrand, "Advanced Calculus for Applications", Second edition, Prentice Hall, 1976.
  12. R.M. James, "On the Remarkable Accuracy of the Vortex Lattice Discretization in Thin Wing Theory", Report DAC-67211, Feb 1969, McDonnell Douglas Corporation, Long Beach, CA.
  13. T.P. Kalman, W.P. Rodden, J.P. Giesing, "Application of the Doublet Lattice Method to Nonplanar Configurations in Subsonic Flow", AIAA Journal of Aircraft, Vol.8, No.6, pp406-413, June 1971.
  14. Krishnomurty Karamcheti, "Principles of Ideal-Fluid Aerodynamics", Robert E. Krieger Publishing Co., Malabar, Florida, 1980. Reprinted by permission of John Wiley & Sons, 1966.
  15. Arnold M. Kuethe and Chuen-Yen Chow, "Foundation of Aerodynamics, Bases of Aerodynamic Design", 3rd edition, 1976, John Wiley & Sons.
  16. M. T. Landahl, "Kernal Function for Nonplanar Oscillating Surfaces in a Subsonic Flow", ALAA Journal, Vol. 5, No. 5, p 1045, May 1967.
  17. B. Laschka, "Zur Theorie der harmonic schwingen den tragen den Flache bei Unterschallanstromung", Zeitschrift fUr Flugwissenschaften, Vol. 1, No. 7, July 1963, pp 265-292.
  18. H. W. Leipmann and A. Roshko, "Elements of Gasdynamics", 1957, John Wiley & Sons.
  19. K. W. Mangler, "Improper Integrals in Theoretical Aerodynamics", Report No:AERO.2424. Royal Aircraft Establishment, 1963.
  20. Benjamin Smilg and Lee S. Wasserman, "Application of Three-Dimensional Flutter Theory to Aircraft Strucumres", AF Technical Report No. 4798, July 1942.
  21. T. Ueda and E. H. Dowell, "A New Solution Method for Lifting Sfurfaces in Subsonic Flow", AIAA Journal, Vol. 20, No. 3, March 1982, pp. 348-355
  22. Marc H. Williams, Karl G. Guderley and Mark RI Let, "An Alternative Derivation for an Integral Equation for Linearized Subsonic Flow Over a Wing", WVRDC-TR-89-3097, August 1989.