Items where Author is "Mukherjee, Somenath"

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Mukherjee, Somenath and Manju, S (2011) An improved parametric formulation for the variationally correct distortion immune three-noded bar element. Structural Engineering and Mechanics . ISSN 1225-4568

Mukherjee, Somenath and Manju, S (2011) An improved parametric formulation for the variationlly correct distortion immune three-noded bar element. Structural Engineering and Mechanics, 38 (3). 000-000.

Mukherjee, Somenath and Manjuprasad, M and Raghunath, Ganesh and Anoop, AM and Onkar, AK (2009) Study of airfoil flutter. Technical Report. National Aerospace Laboratories, Bangalore, India.

Mukherjee, Somenath and Prathap, Gangan (2009) Lectures in FEA (Fundamentals) Lecture 1- Finite Element Analysis using Simple Elements. [Lectures/Presentation]

Mukherjee, Somenath and Prathap, Gangan (2009) Lectures in FEA (Fundamentals) Lecture 2 - Variational Principles in Computational Solid Mechanics. [Lectures/Presentation]

Mukherjee, Somenath and Prathap, Gangan (2009) Lectures in FEA (Fundamentals) Lecture 3 - The best-fit paradigm of FEA: Shadows of the exact. [Lectures/Presentation]

Mukherjee, Somenath and Prathap, Gangan (2009) Lectures in FEA (Fundamentals) Lecture 4 - Special topics of FEA. [Lectures/Presentation]

Mukherjee, Somenath and Manjuprasad, M and Sharma, NK and Rana, Davinder and Onkar, AK (2008) Time domain simulation of airfoil flutter in the subsonic regime using fluid structure coupling through panel method. Technical Report. National Aerospace Laboratories, Bangalore, India.

Mukherjee, Somenath and Manjuprasad, M and Sakravarthini, Deepa S and Avinash, R (2008) Finite element studies on supersonic panel flutter under high thermal environment with arbitrary flow direction. In: Proceedings of the International Conference on Aerospace Science and Technology (INCAST 2008-058), 26-28 Jun 2008, Bangalore, India.

Mukherjee, Somenath and Manjuprasad, M and Avinash, R and Sakravarthini, Deepa S (2007) Finite element studies on supersonic panel flutter under high thermal environment with arbitrary flow direction. Technical Report. National Aerospace Laboratories, Bangalore, India.

Mukherjee, Somenath and Deepa, N and Avinash, R and Manjuprasad, M and Viswanath, S (2007) Analytical investigation of supersonic panel flutter under thermal environment with arbitrary flow direction. Technical Report. National Aerospace Laboratories, Bangalore, India.

Mukherjee, Somenath and Prakash, B M Shashi and Alok, P Burgul and Viswanathan, S (2007) A method for dynamic characterization and response predication using ground vibration test(GVT) data for unknown structure. Technical Report. National Aerospace Laboratories, Bangalore, India.

Mukherjee, Somenath and Deepak , KN (2005) A 4-Dof Whirl Flutter Analysis Of Tractor And Pusher (SARAS) Type Propeller Nacelle System Of Aircraft. Technical Report. NAL, Bangalore.

Mukherjee, Somenath and Deepak , K.N (2005) A 4-Dof Whirl Flutter Analysis Of Tractor And Pusher (Saras) Type Propeller Nacelle System Of Aircraft. Technical Report. NAL, Bangalore.

Mukherjee, Somenath and Arvind , BG (2005) A Theoretical Formulation For Flutter Analysis Of A Typical Subsonic Aircraft Wing (SARAS) Using Quasi-Steady Aerodynamic Theory. Technical Report. NAL, Bangalore.

Mukherjee, Somenath and Prathap, Gangan (2002) Analysis of delayed convergence in the three-noded Timoshenko beam element using the function space approach. Sadhana - Academy Proceedings in Engineering Sciences, 27 (5). pp. 507-526.

Mukherjee, Somenath and Prathap, Gangan (2001) Analysis of shear locking in Timoshenko beam elements using the function space approach13; 13;. In: 2nd International Conference on Theoretical, Applied, Computational and Experimental Mechanics, 27-30 Dec 2001, Kharagpur, India.

Mukherjee, Somenath and Prathap, Gangan (2001) Analysis of shear locking in Timoshenko beam elements using the function space approach. Communications in Numerical Methods in Engineering, 17 (6). pp. 385-393.

This list was generated on Wed Oct 22 01:52:41 2014 IST.