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A method for transonic wind-tunnel corrections.

Authors: Antonio Ferri; Paolo Baronti;

A method for transonic wind-tunnel corrections.

Abstract

14 Lighthill, M. J., "The Hodograph Transformation in Trans-sonic Flow," Proceedings of the Royal Society, London, Ser. A, Vol. 191, 1947, pp. 323-369, Vol. 192, 1948, pp. 135-142. Goldstein, S., Lighthill, M. J., and Craggs, J. W., "On the Hodograph Transformation for High-Speed Flow," The Quarterly Journal of Mechanics and Applied Mathematics, Vol. 1, 1948, pp. 344357 and pp. 442^50. 16 Garabedian, P. R. and Korn, D. G., "Numerical Design of Transonic Airfoils," Numerical Solution of Partial Differential Equations II, Academic Press, New York, 1971, pp. 253-271. 17 Cahn, M. S. and Garcia, J. R., "Transonic Airfoil Design," Journal of Aircraft, Vol. 8, No. 2, Feb. 1971, pp. 84-88. 18 Gretler, W., "Eine indirekte Methode zur Berechnung der ebenen Unterschallstromung," Journal de Mecanique, Vol. 7, No. 1, Jan. 1968, pp. 83-94. 19 Sobieczky, H., "Exakte Losungen der ebenen gasdynamischen Gleichungen in Schallnahe," Zeitschriftfur Flugwissenschaften, Bd. 19, Heft 5, May 1971, pp. 197-214. 20 Sato, J., "Application of Dorodnitsyn's Technique to Compressible Two-Dimensional Airfoil Theories at Transonic Speeds," NAL TR-220T, Oct. 1970, National Aerospace Lab., Tokyo, Japan. 21 Belotserkovskii, O. M. and Chushkin, P. I., "The Numerical Solution of Problems in Gas Dynamics," Basic Developments in Fluid Dynamics, Vol. 1, edited by M. Holt, Academic Press, 1965, pp. 34-89. 22 Dorodnitsyn, A. A., "A Contribution to the Solution of Mixed Problems of Transonic Aerodynamics," Advances in Aeronautical Sciences, Vol. 2, 1959, edited by T. von Karman, Pergamon Press, New York, pp. 832-844. 23 Tai, T. C, "Application of the Method of Integral Relations to Transonic Airfoil Problems," AIAA Paper 71-98, New York, 1971. 24 Melnik, R. E. and Ives, D. C., "Subcritical Flows Over TwoDimensional Airfoils by a Multi-Strip Method of Integral Relations," Grumman Research Dept. Rept. RE-393J, 1970, Grumman Aircraft Co., Bethpage, N. Y. 25 Holt, M. and Masson, B. S., "The Calculation of High Subcritical Flow Past Bodies by the Method of Integral Relations," Proceedings of the Second International Conference on Numerical Methods in Fluid Dynamics, Springer-Verlag, Berlin, Lecture Notes in Physics, Vol. 8, 1971, pp. 207-214. 26 Lee, E. S., "Quasilinearization," Quasilinearization and Invariant Embedding, Academic Press, New York, 1968, Chap. II, pp. 9-39. 27 Ferrari, C. and Tricomi, F. G., "Problems Stemming from the Presence of a Shock in the Transonic Flow about an Airfoil," Transonic Aerodynamics, Academic Press, New York, 1968, pp. 314364. 28 Serrin, J., "Mathematical Principles of Classical Fluid Mechanics," Handbuch der Physik, Springer-Verlag, Berlin, Bd. 8/1, 1959, pp. 190-191. 29 Gill, S., "A Process for the Step-by-Step Integration of Differential Equations in an Automatic Digital Computing Machine," Proceedings of Cambridge Philosophical Society, Vol. 47, 1951, pp. 96-108.

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selected citations
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This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Citations provided by BIP!
popularity
This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
BIP!Popularity provided by BIP!
influence
This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Influence provided by BIP!
impulse
This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.
BIP!Impulse provided by BIP!
37
Average
Top 1%
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