Panel methods in computational fluid dynamics

Annual Review of Fluid Mechanics

Volumn 22, Issue 1, 1990, Pages 255-274

  Hess, J L ^a  

^a BOEING COMPANY   (United States)

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EID: 0000589993     PISSN: 00664189     EISSN: None     Source Type: Book Series    
DOI: 10.1146/annurev.fl.22.010190.001351     Document Type: Article

References (26)

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2. Clark, R. W. 1985. A new iterative matrix solution procedure for three-dimensional panel methods. AIAA Pap. No. 85-0176
3. Dawson, C. W. 1977. A practical computer method for solving ship wave problems. Proc. Int. Conf. Numer. Ship Hydrodyn., 2nd, Berkeley, Calif., pp. 30-38
4. Fei, X. 1984. Calculation of potential flow with a free surface. Rep. No. 2912-1, SSPA, Gothenburg, Swed.
5. Greeley, D. S., Kerwin, J. E. 1982. Numerical methods for propeller design and analysis in steady flow. Soc. Nav. Archit. Mar. Eng. Trans. 90: 415-53
6. Hess, J. L. 1973. Higher-order numerical solution of the integral equation for the two-dimensional Neumann problem. Comput. Methods Appl. Mech. Eng. 2: 1-15
7. Hess, J. L. 1974. The problem of three-dimensional lifting flow and its solution by means of surface singularity distribution. Comput. Methods Appl. Mech. Eng. 4: 283-319. See also, 1972, Rep. MDC-J5679, McDonnell Douglas Aircraft Co., Long Beach, Calif.
8. Hess, J. L. 1975. Improved solution for potential flow about arbitrary axisymmetric bodies by use of a higher-order surface source method. Comput. Methods Appl. Mech. Eng. 5: 297-308
9. Hess, J. L. 1986. Review of the source panel technique for flow computation. In Innovative Numerical Methods in Engineering, ed. R. P. Shaw, J. Periaux, A. Chaudouet, J. Wu, C. Marino, C. A. Brebbia, pp. 197-210. Berlin/Heidelberg: Springer-Verlag
10. Hess, J. L., Smith, A. M. O. 1964. Calculation of nonlifting potential flow about arbitrary three-dimensional bodies. J. Ship Res. 8: 22-44
11. Hess, J. L., Smith, A. M. O. 1966. Calculation of potential flow about arbitrary bodies. Prog. Aeronaut. Sci. 8: 1-138
12. Hess, J. L., Valarezo, W. O. 1985. Calculation of steady flow about propellers using a surface panel method. AIAA J. Propuls, Power 1: 470-76
13. Hess, J. L., Friedman, D. M., Clark, R. W. 1985. Calculation of compressible flow about three-dimensional inlets with auxiliary inlets, slats, and vanes by means of a panel method. NASA CR-174975
14. Johnson, F. T. 1980. A general panel method for the analysis and design of arbitrary configurations in incompressible flows. NASA CR-3079
15. Kerwin, J. E., Kinnas, S. A., Lee, J. T., Shih, W. Z. 1987. A surface panel method for the hydrodynamic analysis of ducted propellers. Soc. Nov. Archit. Mar. Eng. Trans. 95: 93-122
16. Lamb, H. 1932. Hydrodynamics. London: Cambridge Univ. Press. 6th ed.
17. Margason, R. J., Kjelgaard, S. O., Sellers, W. L., Morris, C. E., Walkey, K. B., Shields, E. W. 1985. Subsonic panel methods - a comparison of several production codes. AIAA Pap. No. 85-0280
18. Maskew, B. 1982. Prediction of subsonic aerodynamic characteristics: a case for low-order panel methods. J. Aircr. 19: 157-63
19. Miranda, L. R. 1985. Reply by author to J. L. Hess. J. Aircr. 22: 352
20. Morino, L., Luo, C. C. 1974. Subsonic potential aerodynamics for complex configurations. A general theory. AIAA J. 12: 191-97
21. Newman, J. N. 1985. Algorithms for the free-surface Green's function. J. Eng. Math. 19: 57-67
22. Oskam, B. 1985. Transonic panel method for the full potential equation applied to multicomponent airfoils. AIAA J. 23: 1327-34
23. Slooff, J. W. 1984. On wings and keels. NLR MMP 84006U
24. Smith, A. M. O., Pierce, J. 1958. Exact solution of the Neumann problem. Calculation of plane and axially symmetric flows about or within arbitrary boundaries. Proc. U.S. Natl. Congr. Appl. Mech., 3rd, Providence, R.I., pp. 807-15
25. Tinoco, E. N., Ball, D. N., Rice, F. A. 1987. PAN AIR analysis of a transport high-lift configuration. J. Aircr. 24: 181-86
26. Valarezo, W. O., Hess, J. L. 1986. Timeaveraged subsonic propeller flowfield calculations. AIAA Pap. No. 86-1807-CP