Items where Author is "Subramanian, NR"

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Number of items: 25.

Conference or Workshop Item

Subramanian, NR and Siddalingappa, SR (1986) Computations with 3-D Euler code for wings. In: 2nd National Conference on Aerodynamics, 19-20 Dec 1986, Bangalore, India.

Journal Article

Subramanian, NR and Siddalingappa, SR (1986) Computations with 3-D Euler code for wings. Journal of Aeronautical Society of India, 38 . pp. 241-248.

Subramanian, NR and Chakrabartty, SK (1986) Transonic potential flow computations around finite wings. Journal of Aeronautical Society of India, 38 . pp. 55-57.

Chakrabartty, SK and Subramanian, NR (1980) Low-frequency and small perturbation equation for transonic flow past wings. AIAA Journal, 18 . pp. 1147-1149. ISSN 0001-1452

Ramakrishnan, SV and Subramanian, NR (1978) Flow past nonconical wings with separation. Journal of Aircraft, 15 . pp. 383-384. ISSN 0021-8669

Subramanian, NR (1965) Application of rheoelectrical analogy to the study of wind tunnel contraction (Wind tunnel contraction study of inviscid incompressible flow using rheoelectrical analogy, discussing experimental techniques, contour velocity distribution, optimum smoke injector and adverse pressure gradient estimation). Aeronautical Society of India, Journal, 17 . pp. 154-166.

Subramanian, NR and Tirumalesa, D (1963) A note on the prediction of the shock-wave position on airfoils at transonic speeds (Sinnott technique for predicting shock wave position on airfoils at transonic speeds). Aeronautical Society of India, Journal, 15 . pp. 53-65.

Proj.Doc/Technical Report

Prabhu, DK and Subramanian, NR and Saxena, SK (1993) Hypersonic viscous flow computations using parabolized navier-stokes equations. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Subramanian, NR and Ravishankar, S (1991) Hypersonic flow computations. Technical Report. National Aerospace Laboratories, Bangalore, India.

Chakrabartty, SK and Subramanian, NR (1989) Computation of 3-D transonic flows for wings and wing-body configurations (Closure Report)13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Chakrabartty, SK and Subramanian, NR (1989) Computation of 3-D transonic flows for wings and wing-body13; configurations (Annual Progress Report). Technical Report. National Aeronautical Laboratory, Bangalore, India.

Kannan, SM and Purohit, SC and Subramanian, NR (1988) Algebraic grid generation for missile-type configurations. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Chakrabartty, SK and Subramanian, NR (1988) Computation of 3-D transonic flows for wings and wing-body configurations. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Chakrabartty, SK and Subramanian, NR and Siddalingappa, SR and Das, AK (1987) Computation of 3-D Transonic Flow for Wings and Wing Body13; Configuration. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Subramanian, NR and James, M (1987) On 3D boundary layer computations on swept wings. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Chakrabartty, SK and Subramanian, NR (1986) Computation of 3-D transonic flows for wings and wing body configuration, annual progress report. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Chakrabartty, SK and Subramanian, NR (1986) Computation of transonic potential flows. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Subramanian, NR and Chakrabartty, SK (1985) Transonic flow computations around finite wings. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Subramanian, NR and Chakrabartty, SK (1984) Computation of inviscid transonic flow past aerofoils using body fitted coordinates. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prasad, Simha DS and Subramanian, NR (1979) Computation of aerodynamic characteristics of finite wings in steady supersonic flow. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Subramanian, NR and Ramakrishnan, SV (1977) Dynamic stability derivatives of missile configurations (Theoretical evaluation). Technical Report. National Aeronautical Laboratory, Bangalore, India.

Gopinath, R and Subramanian, NR (1970) Study of the asymptotic behaviour of compressible laminar boundary layers of a dissociating gas. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Gopinath, R and Subramanian, NR (1968) Asymptotic theory of the blunted wedge at hypersonic speeds. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Murthy, KNV and Subramanian, NR (1968) Non equlibrium transonic flow past slender bodies. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Subramanian, NR and Dwarakanath, GS (1966) Hypersonic flow around a blunt body - real gas effects. Technical Report. National Aeronautical Laboratory, Bangalore, India.

This list was generated on Mon Nov 24 03:34:43 2014 IST.