Items where Author is "Chakrabartty, SK"

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Singh, Manish K and Dhanalakshmi, K and Chakrabartty, SK (2007) Navier-stokes analysis of airfoils with gurney flap. Journal of Aircraft, 44 (5). pp. 1487-1493.

Singh, Manish K and Dhanalakshmi, K and Chakrabartty, SK (2006) Navier-stokes analysis of airfoils with Gurney flap. In: 9th Proceedings of AeSI CFD symposium, 11-12 Aug 2006, Bangalore, India.

Dhanalakshmi, K and Mathur, JS and Chakrabartty, SK (2006) Pr-Processing of MiG-29 Aircraft for CFD Analysis. Technical Report. NAL, Bangalore.

Singh, Manish K and Dhanalakshmi, K and Chakrabartty, SK (2006) Navier-Stokes Analysis of Airfoils with Gurney Flap. Project Report. National Aerospace Laboratories, Bangalore.

Chakrabartty, SK (2005) Role Of Computational Fluid Dynamics In The Design Of Aerospace Configurations. Journal of Aerospace Sciences amp; Technology, 57 (1). pp. 24-32. ISSN 0971-950X

Chakrabartty, SK and Dhanalakshmi, K and Ramesh, V (2003) Navier-stokes analysis of GA(W)-2 aerofoil with deflected flap and redesign of Hansa flap for better performance. Computational Fluid Dynamics Journal, 12 (1). pp. 89-97. ISSN 0918-6654

Dhanalakshmi, K and Mathur, JS and Chakrabartty, SK (2003) Radomes for JAGUAR aircraft: Closure Report. Technical Report. National Aerospace Laboratories, Bangalore.

Dhanalakshmi, K and Mathur, JS and Chakrabartty, SK (1999) Euler Computation for a Wing with Aileron Deflection. Technical Report. National Aerospace Laboratories, Bangalore, India.

Hazra, SB and Chakrabartty, SK and Niyogi, P (1999) Compressible viscous flow past aerofoils using a non-oscillatory finite-volume scheme. Computational Fluid Dynamics Journal, 8 (3). pp. 400-409.

Mathur, JS and Dhanalakshmi, K and Chakrabartty, SK (1996) Euler Computations for the GSLV Using the JUEL3D Code. Technical Report. National Aerospace Laboratories, Bangalore, India.

Chakrabartty, SK and Dhanalakshmi, K and Mathur, JS (1995) Computation of Three-Dimensional Transonic Viscous Flow using the JUMBO3D Code. Technical Report. National Aerospace Laboratories, Bangalore, India.

Chakrabartty, SK and Dhanalakshmi, K (1995) Computation of transonic flows with shock-induced separation using algebraic turbulence models. AIAA Journal, 33 (10). pp. 1979-1981.

Chakrabartty, SK and Dhanalakshmi, K (1994) Computation of viscous transonic flows with shocks. Technical Report. National Aerospace Laboratories, Bangalore, India.

Chakrabartty, SK and Dhanalakshmi, K and Mathur, S (1994) Euler Computation for a Multi-Body Launch Vehicle. Technical Report. National Aerospace Laboratories, Bangalore, India.

Chakrabartty, SK and Dhanalakshmi, K and Mathur, JS (1994) Computation of Three- Dimensional Transonic Flow Using a Cell Vertex Finite Volume Method for the Euler Equations. Technical Report. National Aerospace Laboratories, Bangalore, India.

Mathur, JS and Chakrabartty, SK (1994) Approximate factorization scheme for elliptic grid generation with control functions. Numerical Methods for Partial Differential Equations, 10 (6). pp. 703-713.

Chakrabartty, SK and Dhanalakshmi, K (1993) A vertex-based finite-volume algorithm for the Navier-Stokes equations. In: Proceedings of the Fluid Dynamics Symposium in Honour of Professor R. Narasimha on his 60th Birthday, 9 July 1993, Sikkim, India.

Chakrabartty, SK and Desai, SS and Prabhu, DK and Saxena, SK and Majumdar, S (1993) Fluid Dynamics Symposium in honour of Professor R.Narasimha on his 60th birthday. In: Proceedings of the Fluid Dynamics Symposium in Honour of Professor R. Narasimha on his 60th Birthday, 9 Jul 1993, Bangalore, India.

Mathur, JS and Chakrabartty, SK (1993) Grid generation package for high aspect ratio wings. In: Proceedings of the Fluid Dynamics Symposium in Honour of Professor R. Narasimha on his 60th Birthday, 1993, Sikkim.

Mathur, JS and Chakrabartty, SK (1992) An approximate factorisation scheme for elliptic grid generation with control functions. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Chakrabartty, SK (1992) Approximate factorization scheme for transonic potential flow computations. Sadhana, 17 (2). pp. 299-313. ISSN 0256-2499

Chakrabartty, SK (1990) Vertex-based finite-volume solution of the two-dimensional Navier-Stokes equations. AIAA Journal, 28 (10). pp. 1829-1831. ISSN 0001-1452

Chakrabartty, SK (1989) Computation of transonic potential flow RAE-wing-A and body-B2 combination. Technical Report. National Aeronautical Laboratory, 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.

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.

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

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.

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

This list was generated on Mon Nov 24 03:48:00 2014 IST.