Narasimha was born on 20 July 1933. He was born in a Kannada family tracing its origins toRoddam, a village in theAnantapur district ofAndhra Pradesh.[9] His father, R.L. Narasimhaiah, was a professor of physics in Bangalore'sCentral College, and was also aKannada language science writer with a focus on physics and astronomy.[10]
Narasimha started his research career atCaltech, working on the problem ofjet engine noise reduction. After the launch of the RussianSputnik and the resulting interest in space programs, he shifted focus torarefied gas andfluid dynamics, working withHans W. Liepmann.[13] He continued this research at theNASA Jet Propulsion Laboratory, where he went on to study aerodynamics and supersonic flows toward better understanding of the structure of shockwaves. During this time, he worked on one of the space agency's first computers.[13]
He returned to India in 1962, and joined theIndian Institute of Science as a professor in its aeronautical engineering department (1962–1999), where he continued his fluid dynamics research, studyingturbulent flow and relaminarisation, including the study of fluid flow from turbulent (chaotic) tolaminar (streamlined) forms.[13] In 1970, he was a member of the investigation team underSatish Dhawan that studied the airworthiness ofIndian AirlinesAvro 748.[13][14]
During his time at theNational Aerospace Laboratories, Narasimha led the research initiative intoparallel computing as a means to solve fluid dynamics problems.[13][17] His efforts lead to first parallel computer in India and development of a code for weather prediction of tropical regions. He was also a contributing member to the team that designed thelight combat aircraft.[18]
Over the course of his six decade long academic career he has made significant contributions to fundamental and applied fluid dynamics. At the Indian Institute of Science, his research included the 'bursting' phenomenon in a turbulent boundary layer,[19] non-linear vibration of an elastic string,[20] equilibrium and relaxation in turbulent wakes,[21] relaminarization,[22] hydrodynamic instability,[23] wall jets[24] and the study of clouds[25][26] as volumetrically heated jets. At the Engineering Mechanics Unit of the Jawaharlal Nehru Centre for Advanced Scientific Research, Narasimha continued his research on fluid dynamics of clouds via laboratory experiments[27] as well as numerical simulations.[28] He also studied gas turbine blades,[29] turbulent free shear layers[30] and proposed a novel wing design for turboprop aircraft.[31]
He was the longest-serving member of the Indian Space Commission, a policy-making body for space exploration in India.[13] He resigned from this position in February 2012, in protest at the blacklisting of three former ISRO technocrats includingG. Madhavan Nair, former ISRO chairman, for their perceived role in a controversial agreement between ISRO's commercial entityAntrix and Devas Multimedia in 2005.[32][33]
The President, Shri Pranab Mukherjee presenting the Padma Vibhushan Award to Prof. Roddam Narasimha, at an Investiture Ceremony-II, at Rashtrapati Bhavan, in New Delhi on 20 April 2013
^Narayan, K Yegna; Narasimha, R (August 1973). "Parametric Analysis of Turbulent Wall Jets".Aeronautical Quarterly.24 (3):207–218.doi:10.1017/s0001925900006600.ISSN0001-9259.
^Rao, Samrat; Vybhav, G. R.; Prasanth, P.; Deshpande, S. M.; Narasimha, R. (2020), "A DNS Study of Bulk Flow Characteristics of a Transient Diabatic Plume that Simulates Cloud Flow",Recent Advances in Theoretical, Applied, Computational and Experimental Mechanics, Lecture Notes in Mechanical Engineering, Singapore: Springer Singapore, pp. 387–396,doi:10.1007/978-981-15-1189-9_31,ISBN978-981-15-1188-2,S2CID216430546
^Ranjan, Rajesh; Deshpande, S.M.; Narasimha, Roddam (August 2017). "New insights from high-resolution compressible DNS studies on an LPT blade boundary layer".Computers & Fluids.153:49–60.doi:10.1016/j.compfluid.2017.05.004.ISSN0045-7930.
^[1], "Optimal wing planforms for reducing the induced or total drag of the wing of an aircraft driven by wing-mounted tractor propellers/rotors", issued 5 July 2010