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11 - Satish Dhawan

Published online by Cambridge University Press:  07 October 2011

Roddam Narasimha
Affiliation:
Jawaharlal Nehru Centre for Advanced Scientific Research
Peter A. Davidson
Affiliation:
University of Cambridge
Yukio Kaneda
Affiliation:
Nagoya University, Japan
Keith Moffatt
Affiliation:
University of Cambridge
Katepalli R. Sreenivasan
Affiliation:
New York University
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Summary

Introduction

Satish Dhawan was born on 25 September 1920 in Srinagar, Kashmir, the home town of his mother Lakshmi. His father, Devidayal, was from the North Western Frontier Province; both parents came from professional families, full of doctors, lawyers and academics – Devidayal retired as a respected judge of the High Court in Lahore, now in Pakistan. Satish's education began under private tutors at home, as his father kept getting transferred in his early career from one town to another in the North West (Kipling country to Indo-British readers). He completed his Indian education at the University of Punjab in Lahore with an unusual combination of degrees: BA in physics and mathematics (1938), MA in English literature (1941) and BE (Hons.) in mechanical engineering (1945). In 1946 he sailed to the USA on a government scholarship, and obtained an MS in aeronautical engineering from the University of Minnesota the following year. (The summer of 1947 saw much turmoil in the subcontinent preceding its imminent partition, and Satish's parents reluctantly left Lahore for India – never to return – a week before the formal end of colonial rule.) In the USA Satish moved to the California Institute of Technology where, with Hans W. Liepmann as his adviser, he obtained the degree of Aeronautical Engineer in 1949 and a PhD in aeronautics and mathematics in 1951. Dhawan made a strong impression, scientifically and otherwise, on everybody he came in contact with at Caltech.

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Publisher: Cambridge University Press
Print publication year: 2011

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References

Abu-Ghannam, B.J. and Shaw, R. 1980. Natural transition of boundary layers – the effects of turbulence, pressure gradient and flow history. J. Mech. Engg. Sci. 22, 213–228.CrossRefGoogle Scholar
Ackeret, J., Feldmann, F. and Rott, N. 1946. Inst. Aerodyn. ETH, Report no. 10.
Adamson, T.C. Jr. and Messiter, A.F. 1980. Analysis of two-dimensional interactions between shock waves and boundary layers. Ann. Rev. Fluid Mech. 12, 103–138.CrossRefGoogle Scholar
Coles, D.E. 1953. Measurements in the boundary layer on a smooth flat plate in super-sonic flow. PhD thesis, Caltech.
Coles, D.E. 1954a. Measurements of turbulent friction on a smooth flat plate in super-sonic flow. J. Aero Sci. 21, 433–448.CrossRefGoogle Scholar
Coles, D. 1954b. The problem of the turbulent boundary layer. ZAMP 5, 182–203.CrossRefGoogle Scholar
Dhawan, S. 1953. Direct measurements of skin friction. NACA Report 1121.
Dhawan, S. 1981. A glimpse of fluid mechanics research in Bangalore 25 years ago. Proc. Ind. Acad. Sci. (Engg. Sci.) 4, 95–109.Google Scholar
Dhawan, S. and Narasimha, R. 1958. Some properties of boundary layer flow during transition from laminar to turbulent motion. J. Fluid Mech. 3, 418–436.CrossRefGoogle Scholar
Dryden, H.L. 1936. Air flow in the boundary layer near a plate. NACA Report 562.
Dryden, H.L. 1953. Review of published data on the effect of roughness. J. Aero. Sci. 20, 477–482.CrossRefGoogle Scholar
Emmons, H.W. 1951. The laminar-turbulent transition in a boundary layer – Part I.J. Aero. Sci. 18, 490–498.CrossRefGoogle Scholar
Emmons, H.W. and Bryson, A.E. 1952. The laminar-turbulent transition in a boundary layer (Part II). Proc. 1st US Natl. Cong. Appl. Mech., 859–868.Google Scholar
Kármán, von, T. 1936. The problem of resistance in compressible fluids. Att. dei Convegni 5, R., Accad. d'Italia, pp. 222–277.Google Scholar
Liepmann, H.W. 1943. Investigations in laminar boundary-layer stability and transition on curved boundaries. NACA ACR 3H30.
Liepmann, H.W. 1945. Investigation of boundary layer transition on concave walls. NACA ACR 4J28.
Liepmann, H.W. 1946. The interaction between boundary layer and shock waves in transonic flow. J. Aero. Sci. 13, 623–637.CrossRefGoogle Scholar
Liepmann, H.W. 2002. Remembering Satish Dhawan. Engineering & Science (Caltech) 65(4), 41–43.Google Scholar
Liepmann, H.W., Roshko, A. and Dhawan, S. 1951. On reflection of shock waves from boundary layers. NACA Report 1100.
Marusic, I., McKeon, B.J., Monkewitz, P.A., Nagib, H.M., Smits, A.J. and Sreenivasan, K.R. 2010. Wall-bounded turbulent flows at high Reynolds numbers: recent advances and key issues. Phys. Fluids 22, 065103.CrossRefGoogle Scholar
Narasimha, R. 1957. On the distribution of intermittency in the transition region of a boundary layer. J. Aero. Sci. 24, 711–712.Google Scholar
Narasimha, R. 1958. A study of transition from laminar to turbulent flow in the boundary layer of a flat plate. AIISc thesis, Dept. Aero. Eng., Ind. Inst. Sci., Bangalore.Google Scholar
Narasimha, R. 1985. The laminar–turbulent transition zone in the boundary layer. Prog. Aerospace. Sci. 22, 29–80.CrossRefGoogle Scholar
Narasimha, R. 2002. Satish Dhawan. Current Science 82, 222–225.Google Scholar
Narasimha, R. and Deshpande, S.M. 1982. Surveys in Fluid Mechanics. Indian Academy of Sciences, Bangalore.Google Scholar
Reynolds, O. 1883. An experimental investigation of the circumstances which determine whether the motion of water shall be direct or sinuous and of the law of resistance in parallel channels. Phil. Trans. Roy. Soc. A 174, 935–982.CrossRefGoogle Scholar
Schlichting, H. 1955. Boundary Layer Theory. Pergamon Press.Google Scholar
Schubauer, G.B and Klebanoff, P.S. 1955. Contributions on the mechanics of boundary-layer transition. NACA Tech. Note 3489.
Shultz-Grunow, F. 1940. Neues Reibungswiderstandsgesetz für glatte Platten. Luftfahrtforschung, 17, 239–246. Available in English as NACA Tech. Mem. 986 (1941).Google Scholar
Wygnanski, I.J., Haritonidis, J.H. and Kaplan, R.E. 1979. On a Tollmien–Schlichting wave packet produced by a turbulent spot. J. Fluid Mech. 92, 505–528.CrossRefGoogle Scholar

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