Number of items: **33**.

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 **Sat Apr 25 03:51:41 2015 IST**.