Abstract
Four principal questions are discussed.
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(1)
Under what conditions are the aerodynamic forces essentially linear functions of the airfoil motion?.
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(2)
Are there viable alternative methods to finite difference procedures for solving the relevant fluid dynamical equations?.
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(3)
Under those conditions when the aerodynamic forces are non-linear functions of the airfoil motion, what is the significance of the multiple (nonunique) solutions which are sometimes observed?.
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(4)
What are effective, efficient computational procedures for using unsteady transonic aerodynamic computer codes in aeroelastic (e.g., flutter) analyses?.
This work is supported by AFOSR Grant 81-0213A. Dr. Anthony Amos is the technical monitor.
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References
Albano, E. and W. P. Rodden. “A Doublet Lattice Method for Cal-culating Lift Distribution on Oscillating Wings in Subsonic Flows,” AIAA Journal, 7 (1969), 279–85.
Ballhaus, W. F. and Goorjian, P. M. “Implicit Finite Difference Computations of Unsteady Transonic Flows About Airfoils,” AIAA Journal, 15 (1977), 1728–35.
“Efficient Solution of Unsteady Transonic Flows About Airfoils,” Paper 14, AGARD Conference Proceedings No. 226, Unsteady Airload in Separated and Transonic Flows, 1978a.
“Computation of Unsteady Transonic Flows by the Indicial Method,” AIAA Journal, 16, No. 2 (1978b), 117–24.
Bauer, R., Garabedian, P., and Korn, D. “Supercritical Wing Sec-tions,” Lecture Notes in Economics and Mathematical Systems, 66, Springer-Verlag, 1972.
Bland, S. R. and Edwards, J. W. “Airfoil Shape and Thickness Effects on Transonic Airloads and Flutter,” AIAA SDM Conference in Lake Tahoe, CA, May 1983, AIAA Paper No. 83–0959.
Borland, C. J. and Rizzetta, D. P. “Transonic Unsteady Aerodynamics for Aeroelastic Applications, I: Technical Development Summary,” AFWAL TR 80–8107, I, June 1982a.
“Nonlinear Transonic Flutter Analysis,” AIAA Journal, 20, No. 11 (1982b), 1606–15.
Borland, C. J., Rizzetta, D. P., and Yoshihara, H. “Numerical Solution of Three-Dimensional Unsteady Transonic Flow Over Swept Wings,” AIAA Journal, 20, No. 3 (1982), 340–47.
Cockey, W. D. “Panel Method for Perturbations of Transonic Flows With Finite Shocks,” Ph.D. thesis, Princeton University, June 1983.
Davis, S. S. and Malcolm, G. “Experiment in Unsteady Transonic Flows,” Proc. of the AIAA/ASME/ASCE 20th Structures, Structural Dynamics and Materials Conference, St. Louis, MO, April 1979.
Dowell, E. H. “A Simple Method for Converting Frequency-Domain Aerodynamics to the Time Domain,” NASA TM 81844, 1980.
Dowell, E. H., Bland, S. R., and Williams, M. H. “Linear/Nonlinear Behavior in Unsteady Transonic Aerodynamics,” AIAA Journal, 21 (1983), 38–46.
Dowell, E. H., Ueda, T., and Goorjian, P. M. “Transient Decay Times and Mean Values of Unsteady Oscillations in Transonic Flow,” AIAA Journal, 21, No. 12 (1983), 1762–64.
Edwards, J. W., et al. “Time-Marching Transonic Flutter Solutions Including Angle-of-Attack Effects,” AIAA Paper 82-0685, presented at the 23rd SDM Conference, New Orleans, LA, May 1982.
Ehlers, F. E. and Weatherill, W. H. “A Harmonic Analysis Method for Unsteady Transonic Flow and its Application to the Flutter of Airfoils,” NASA CR-3537, 1982.
Fung, K. Y., Yu, N. J., and Seebass, R. “Small Unsteady Perturbations in Transonic Flows,” AIAA Journal, 16 (1978), 815–22.
Goldstein, M. E. Aeroacoustics, New York: McGraw-Hill, 1976.
Goorjian, P. M. Private communication, NASA Ames Research Center.
Hessenius, K. A. and Goorjian, P. M. “Validation of LTRAN2-HI by Comparison With Unsteady Transonic Experiment,” AIAA Journal, 20, No. 5 (1982), 731–32.
Hounjet, M.H.L. “A Transonic Panel Method to Determine Loads on Oscillating Airfoils With Shocks,” AIAA Journal, 19 (1981a), 559–66.
“A Field Panel Method for the Calculation of In-viscid Transonic Flow About Thin Oscillating Airfoils With Shocks,” NLR MP 81043 U, National Aerospace Laboratory, Netherlands. Presented at the International Symposium on Aeroelasticity, Nuremburg, October 5–7, 1981b, Germany.
Hoirwink, R. and van der Vooren, J. “Improved Version of LTRAN2 for Unsteady Transonic Flow Computations,” AIAA Journal, 18, No. 8 (1980), 1008–10.
Hsu, J. C. and Meyer, A. U. Modern Control Principles and Applications, New York: McGraw-Hill, 1968.
Isogai, K. “Numerical Study of Transonic Flutter of a Two-Dimensional Airfoil,” Technical Report of National Aerospace Laboratory, Japan, NAL-TR-617T, 1980.
Kerlick, G. D. and Nixon, D. “Mean Values of Unsteady Oscillations in Transonic Flow Calculations,” AIAA Journal, 19, No. 11 (1981), 1496–98.
Lighthill, M. J. “On Boundary Layers and Upstream Influence, II; Supersonic Flows Without Separation,” Proceedings of the Royal Society, A217(1953), 478–507.
Liu, D. D. “A Lifting Surface Theory Based on an Unsteady Linearized Transonic Flow Model,” AIAA Paper 78–501, 1978.
Magnus, R. J. and Yoshihara, H. “Calculation of Transonic Flow Over an Oscillating Airfoil,” AIAA Paper 75–98, Jan. 1975.
McCroskey, W. J. “Unsteady Airfoils,” Annual Review of Fluid Mechanics, 14 (1982), 285–311.
Mcintosh, S. private communication.
Miles, J. W. The Potential Theory of Unsteady Supersonic Flow, Cambridge: Cambridge University Press, 1959, 4–13.
Morino, L. “A General Theory of Unsteady Compressible Potential Aerodynamics,” NASA CR-2464, December 1974.
Morino, L. and K. Tseng. “Time-Domain Green’s Function Method for Three-Dimensional Nonlinear Subsonic Flows,” AIAA Paper 78–1204, 1978.
Murman, E. M. “Analysis of Embedded Shock Waves Calculated by Relaxation Methods,” Proceedings of the AIAA CFD Conference, July 1973, 27–40.
Nixon, D. “Calculation of Unsteady Transonic Flows Using the Integral Equation Method,” AIAA Paper 78–18, January 1978.
“On the Derivation of Universal Indicial Functions,” AIAA Paper 81–0828, Jan. 1981.
Nixon, D. and Kerlick, G. D. “Calculation of Unsteady Transonic Pressure Distributions by Indicial Methods,” Nielsen Engineering and Research Paper 117, 1980.
Rizzetta, D. P. and Borland, C. J. “Unsteady Transonic Flow Over Wings Including Inviscid/Viscous Interactions,” AIAA Journal, 21, No. 3 (1983), 363–71.
Salas, M. D., Jameson, A., and Melnik, R. E. “A Comparative Study of the Nonuniqueness Problem of the Potential Equation,” presented at the 6th AIAA CFD Conference, Danvers, Mass., July 13–15, 1983.
Seebass, R. “Advances in the Understanding and Computation of Unsteady Transonic Flows,” Recent Advances in Aerodynamics, ed. A. Krothapalli and C. Smith, 1984.
Steinhoff, J. and Jameson, A. “Multiple Solutions of the Transonic Potential Flow Equations,” AIAA Paper No. 81–1019, AIAA Computational Fluid Dynamics Conference, Palo Alto, CA, June 1981.
Taylor, R. F., Bogner, F. K., and Stanley, E. C. “A Stability Prediction Method for Nonlinear Aeroelasticity,” AIAA Paper 80-0797, presented at the AIAA/ASME/AHS/ASCE Conference, Seattle, WA, May 12–14, 1980.
Tijdeman, H. “Investigation of the Transonic Flow Around Oscillating Airfoils,” Ph.D. thesis, Delft University, 1977.
Tijdeman, H. and Seebass, R. “Transonic Flow Past Oscillating Airfoils,” Annual Review of Fluid Mechanics, 12 (1980), 181–222.
Tran, C. T. and Petot, M. “Semi-empirical Model for the Dynamic Stall of Airfoils in View of the Application of Responses of a Helicopter Blade in Forward Flight,” Paper 48, Proceedings, 6th European Rotorcraft and Powered-lift Aircraft Forum, Bristol, England, 1980.
Ueda, T. and Dowell, E. H. “Flutter Analysis Using Nonlinear Aero-dynamic Forces,” AIAA Paper 82–0728, 1982.
“Describing Function Flutter Analysis for Transonic Flow: Extension and Comparison With Time Marching Analysis,” AIAA Paper 83–0958, 1983.
Voss, R. “Time-Linearized Calculation of Two-Dimensional Unsteady Transonic Flow at Small Disturbances,” DFVLR FB-81–01, 1981.
Williams, M. H. “Unsteady Thin Airfoil Theory for Transonic Flows With Embedded Shocks,” Department of Mechanical and Aerospace Engineering, Report No. 1876, Princeton University, May 1978; also AIAA Journal, 18 (1980), 615–24; also see “Unsteady Airloads in Supercritical Transonic Flows,” Proceedings of the AIAA/ASME/ ASCE 20th Structures, Structural Dynamics and Materials Conference, St. Louis, MO, April 1979b.
“The Linearization of Transonic Flows Containing Shocks,” AIAA Journal, 17 (1979a), 394–97.
Williams, M. H., et al. “Aerodynamic Effects of Inviscid Parallel Shear Flows,” AIAA Journal, 15, No. 8 (1977), 1159–66.
Yang, T. Y., Guruswamy, P., and Striz, A. G. “Aeroelastic Response Analysis of Two-Dimensional, Single and Two Degree of Freedom Airfoils in Low Frequency, Small-Disturbance Unsteady Transonic Flow,” AFFDL-TR-79–3077, 1979.
“Application of Tran-sonic Codes to Flutter Analysis of Conventional and Supercritical Airfoils,” AIAA SDM Conference in Atlanta, GA, AIAA Paper 81–0603, 1981.
Yang, T. Y., et al. “Flutter Analysis of a NACA 64A006 Airfoil in Small Disturbance Transonic Flow,” J. Aircraft, 17, No. 4 (1980), 225–32.
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Dowell, E.H. (1986). Unsteady Transonic Aerodynamics and Aeroelasticity. In: Krothapalli, A., Smith, C.A. (eds) Recent Advances in Aerodynamics. Springer, New York, NY. https://doi.org/10.1007/978-1-4612-4972-6_2
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DOI: https://doi.org/10.1007/978-1-4612-4972-6_2
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