Comment on “A new solution method for lifting surfaces in subsonic flow”

AIAA Journal

Volumn 22, Issue 1, 1984, Pages 160-

  Rodden, William P ^a  

^a La Cañada Flintridge ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 85002529705     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.8362     Document Type: Article

References (18)

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2. Albano, E., and Rodden, W. P., “A Doublet-Lattice Method for Calculating Lift Distributions on Oscillating Surfaces in Subsonic Flows,” AIAA Journal, Vol. 7, Feb. 1969, pp. 279-285, “Errata,” Nov. 1969, p. 2192.
3. Hedman, S. G., “Vortex Lattice Method for Calculation of Quasi Steady State Loadings on Thin Elastic Wings,” Aeronautical Research Institute of Sweden, Rept. 105, Oct. 1965.
4. Rubbert, P. E., “Theoretical Characteristics of Arbitrary Wings by a Nonplanar Vortex Lattice Method,” The Boeing Company, Seattle, Wash., Rept. D6-9244, 1965.
5. Dulmovits, J., “A Lifting Surface Method for Calculating Load Distributions and the Aerodynamic Influence Coefficient Matrix for Wings in Subsonic Flow,” Grumman Aircraft Engineering Corp., Bethpage, N.Y., Rept. ADR 01-02-64.1, 1964.
6. Belotserkovskii, S. M., The Theory of Thin Wings in Subsonic Flow, Plenum Press, New York, 1967.
7. “Vortex-Lattice Utilization,” NASA SP-405, 1976.
8. Laschka, B., “Zur Theorie der harmonisch schwingenden tragenden Flache bei Unterschallanstromung,” Zeitschrift für Flugwissenschaften, Heft 7, 1963, pp. 265-291.
9. Rowe, W. S., Redman, M. C., Ehlers, F. E., and Sebastian, J. D., “Prediction of Unsteady Aerodynamic Loadings Caused by Leading Edge and Trailing Edge Control Surface Motion in Subsonic Compressible Flow—Analysis and Results,” NASACR-2543, 1975.
10. Schade, T. and Krienes, K., “The Oscillating Circular Airfoil on the Basis of Potential Theory,” NACATM 1098, 1947.
11. Woodcock, D. L., “A Comparison of Methods Used in Lifting Surface Theory,” AGARD Rept. No. 583, Supplement to the AGARD Manual on Aeroelasticity, Part VI, 1971.
12. Försching, H., Triebstein, H., and Wagener, J., “Pressure Measurements on an Harmonically Oscillating Swept Wing with Two Control Surfaces in Incompressible Flow,” Symposium on Unsteady Aerodynamics for Aeroelastic Analyses of Interfering Surfaces, AGARD-CP-80-71, Part II, 1971, pp. 15-1-15-12.
13. Petkas, J. S., “Oscillatory Aerodynamic Representation Using Discrete Load Line Element (DLLE) Method,” Lockheed-Georgia Co., Marietta, Ga., unpublished Memorandum, Feb. 1969.
14. Ashley, H. and Rodden, W. P., “Wing-Body Aerodynamic Interaction,” Annual Review of Fluid Mechanics, Vol. 4, 1972, pp. 431-472.
15. Landahl, M. T., “Kernel Function for Nonplanar Oscillating Surfaces in a Subsonic Flow,” AIAA Journal, Vol. 5, May 1967, pp. 1045-1046.
16. Rodden, W. P., Giesing, J. P., and Kalman, T. P., “Refinement of the Nonplanar Aspects of the Subsonic Doublet-Lattice Lifting Surface Method,” Journal of Aircraft, Vol. 9, Jan. 1972, pp. 69-73.
17. Rodden, W. P., “Comment on ‘Effect of Stabilizer Dihedral and Static Lift on T-Tail Flutter’,” Journal of Aircraft, Vol. 15, July 1978, pp. 447-448.
18. Giesing, J. P., and Kalman, T. P., and Rodden, W. P., “Subsonic Steady and Oscillatory Aerodynamics for Multiple Interfering Wings and Bodies,” Journal of Aircraft, Vol. 9, Oct. 1972, pp. 693-702