Subsonic potential aerodynamics for complex configurations : A general theory

AIAA Journal

Volumn 12, Issue 2, 1974, Pages 191-197

  Morino, Luigi ^a   Kuo, Ching Chiang ^b  

^a BOSTON UNIVERSITY   (United States)

^b MS 23 11   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS;

EID: 0016028440     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.49191     Document Type: Article

References (33)

1. Ashley, H., Widnall, S., and Landahl, M. T. “New Directions in Lifting Surface Theory,” AIAA Journal, Vol. 3, No. 1, Jan. 1965, pp. 3-16.
2. Landahl, M. T. and Stark, V. J. E., “Numerical Lifting-Surface Theory—Problems and Progress,” AIAA Journal, Vol. 6, No. 11, Nov. 1968, pp. 2049-2060.
3. Albano, E. and Rodden, W. P., “A Doublet-Lattice Method for Calculating Lift Distribution on Oscillating Surfaces in Subsonic Flows,” AIAA Journal, Vol. 7, No. 2, Feb. 1969, pp. 279-285.
4. Ashley, H. and Rodden, W. P., “Wing-Body Aerodynamic Interaction,” Annual Review of Fluid Mechanics, Vol. 4, 1972, pp. 431-472.
5. Rubbert, P. E. and Saaris, G. R., “Review and Evaluation of a Three-Dimensional Lifting Potential Flow Analysis Method for Arbitrary Configurations,” AIAA Paper 72-188, San Diego, Calif., 1972.
6. Labrujere, T. E., Loeve, W., and Slooff, J. W., “An Approximate Method for the Calculation of the Pressure Distribution on Wing-Body Combinations at Subcritical Speeds,” AGARD Conference Proceedings 71, Aerodynamic Interference, Sept. 1970.
7. Hess, J. L., and Smith, A. M. O., “Calculation of Potential Flow About Arbitrary Bodies,” Progress in Aeronautical Sciences, Vol. 8, Pergamon Press, New York, 1966.
8. Hess, J. L., “Calculation of Potential Flow About Arbitrary Three-Dimensional Lifting Bodies,” Rept. MDC-J5679-01, Oct. 1972, Douglas Aircraft Co., Long Beach, Calif. "
9. Tulinius, J. R., “Theoretical Prediction of Thick Wing and Pylon-Fanpod-Nacelle Aerodynamic Characteristics at Subcritical Speeds,” Rept. NA-71-447, June 1971, North American Rockwell Corp., El Segundo, Calif.
10. Djojodihardjo, R. H. and Widnall, S. E., “A Numerical Method for the Calculation of Nonlinear Unsteady Lifting Potential Flow Problems,” AIAA Journal, Vol. 7, No. 10, Oct. 1969, pp. 2001-2009.
11. Woodward, F. A., “Analysis and Design of Wing-Body Combinations at Subsonic and Supersonic Speeds,” Journal of Aircraft, Vol. 5, No. 6, Nov.-Dec. 1968, pp. 528-534.
12. Kalman, T. P., Rodden, W. P., and Giesing, J. P., “Application of the Doublet-Lattice Method to Nonplanar Configurations in Subsonic Flow,” Journal of Aircraft, Vol. 8, No. 6, June 1971, pp. 406-413.
13. Giesing, J. P., Kalman, T. P., and Rodden, W. P., “Subsonic Steady and Oscillatory Aerodynamics for Multiple Interfering Wings and Bodies,” Journal of Aircraft, Vol. 9, No. 10, Oct. 1972, pp. 693-702.
14. Baals, D. D., Robins, A. W., and Harris, R. V., Jr., “Aerodynamic Design Integration of Supersonic Aircraft,” Journal of Aircraft, Vol. 7, No. 5, Sept.-Oct. 1970, pp. 385-394.
15. Shrout, B. L., “Extension of a Numerical Solution for the Aerodynamic Characteristics of a Wing to Include a Canard or Horizontal Tail,” AGARD Conference Proceedings 71, Aerodynamic Interference, Sept. 1970.
16. Kariappa K. and Smith, B. C. C., “Development and Applications of Supersonic Unsteady Consistent Aerodynamics for Interfering Parallel Wings,” AIAA Paper 73-317, Williamsburg, Va., 1973.
17. Morino, L., “Unsteady Compressible Potential Flow Around Lifting Bodies Having Arbitrary Shapes and Motions,” TR-72-01, June 1972, Boston Univ., Boston, Mass.
18. Morino, L., “Unsteady Compressible Potential Flow Around Lifting Bodies: General Theory,” AIAA Paper 73-196, Washington, D.C., 1973.
19. Kuo, C. C. and Morino, L., “Steady Subsonic Flow Around Finite-Thickness Wings,” TR-73-02, Feb. 1973, Boston Univ., Boston, Mass.
20. Morino, L. and Kuo, C. C., “Unsteady Subsonic Flow Around Oscillating Finite-Thickness Wings,” TR-73-03, Feb. 1973, Boston Univ., Boston, Mass.
21. Morino, L. and Kuo, C. C., “Unsteady Subsonic Compressible Flow Around- Finite-Thickness Wings,” AIAA Paper 73-313, Williamsburg, Va., 1973.
22. Lamb, Sir H., Hydrodynamics, 6th ed., Dover, New York, 1945, pp. 58-61.
23. Mangler, K. W. and Smith, J. H. B., “Behaviour of the Vortex Sheet at the Trailing Edge of a Lifting Wing,” The Aeronautical Journal of the Royal Aeronautical Society, Vol. 74, Nov. 1970, pp. 906-908.
24. Lessing, H. C., Troutman, J. C., and Menees, G. P., Experimental Determination of the Pressure Distribution on a Rectangular Wing Oscillating in the First Bending Mode for Mach Numbers from 0.24 to 1.30,” TN D-344, 1960, NASA.
25. Cunningham, A. M., Jr., “An Efficient, Steady Subsonic Collocation Method for Solving Lifting-Surface Problems,” Journal of Aircraft, Vol. 8, No. 3, March 1971, pp. 168-176.
26. Hsu, P. T., “Flutter of Low Aspect-Ratio Wings, Part I, Calculation of Pressure Distributions for Oscillating Wings of Arbitrary Platform in Subsonic Flow by the Kernel-Function Methods,” TR-64-1, Oct. 1957, MIT, Cambridge, Mass.
27. Kulakowski, L. J. and Haskell, R. N., “Solution of Subsonic Nonplanar Lifting-Surface Problems by Means of High-Speed Digital Computers,” Journal of Aerospace Sciences, Vol. 28, Feb. 1961, pp. 103-113.
28. Ashley, H. and Landahl, M., Aerodynamics of Wings and Bodies, Addison-Wesley, Reading, Mass., 1965, p. 159.
29. Kolbe, C. D. and Boltz, F. W., “The Forces and Pressure Distribution at Subsonic Speeds on a Planar Wing Having 45° of Sweep Back, an Aspect Ratio of 3, and a Taper Ratio of 0.5,” RMA51G31, Oct. 1951, NACA.
30. Yates, E. C., Jr., private communication, April 1971, Boston, Mass.
31. Laschka, B., “Die Instationaren Luftkräfte an Harmonisch Schwingenden Tragflügeln Endlicher Spannweite Bei Unter-Und Überschallgeschwindigkeit,” Jahrbuch, 1961, der WGL, pp. 207-219.
32. Haviland, J. K., “Downwash-Velocity Potential Method for Lifting Surfaces,” AIAA Journal, Vol. 9, No. 11, Nov. 1971, pp. 2268-2269.
33. Watkins, C. E., Runyan, H. S., and Woolston, D. S., “On the Kernel Function of the Integral Equation Relating the Lift and Downwash Distributions of Oscillating Finite Wings in Subsonic Flow,” Rept. 1234, 1955, NACA (supersedes NACA TN 3131).