1973•AIAA JournalRequires access

A method for transonic wind-tunnel corrections.

Antonio Ferri, PAOLO O. BARONTI

Open publisher page 58 citations

Abstract

14 Lighthill, M. J., 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., Design of 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 Speeds, NAL TR-220T, Oct. 1970, National Aerospace Lab., Tokyo, Japan. 21 Belotserkovskii, O. M. and Chushkin, P. I., Numerical Solution of in Gas 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 of 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 Airfoil Problems, AIAA Paper 71-98, New York, 1971. 24 Melnik, R. E. and Ives, D. C., 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., 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 Flow about an Airfoil, 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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14 Lighthill, M. J., 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., Design of 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 Speeds, NAL TR-220T, Oct. 1970, National Aerospace Lab., Tokyo, Japan. 21 Belotserkovskii, O. M. and Chushkin, P. I., Numerical Solution of in Gas 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 of 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 Airfoil Problems, AIAA Paper 71-98, New York, 1971. 24 Melnik, R. E. and Ives, D. C., 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., 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 Flow about an Airfoil, 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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14 Lighthill, M. J., 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., Design of 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 Speeds, NAL TR-220T, Oct. 1970, National Aerospace Lab., Tokyo, Japan. 21 Belotserkovskii, O. M. and Chushkin, P. I., Numerical Solution of in Gas 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 of 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 Airfoil Problems, AIAA Paper 71-98, New York, 1971. 24 Melnik, R. E. and Ives, D. C., 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., 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 Flow about an Airfoil, 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.

Key concepts: Transonic, Subsonic and transonic wind tunnel, Wind tunnel, Aerospace engineering, Aerodynamics, Mechanics, Meteorology, Aeronautics

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