Items where Author is "Somashekar, BR"

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Number of items: 34.

Somashekar, BR and Rama Murthy, MR and Rajagopal, P and Sundararajan, D and Shashikala, Rajappa and Annamma Samuel, - and Janardhanam, S (1997) Aeroelastic testing of LCA wing models - Model fabrication - Ground testing - Wind tunnel testing and Data analysis. Project Report. National Aerospace Laboratories, Bangalore.

Vijaya Vittala, NG and Barai, A and Kamesh, JV and Viswanath, S and Somashekar, BR (1994) Flutter Characteristics of HANSA2 (NALLA 2C). Technical Report. National Aerospace Laboratories, Bangalore, India.

Somashekar, BR and Rajagopalan, SR and Ramamurthy, MR and Sundararajan, D (1994) Aeroelastic studies at National Aerospace Laboratory: a review. In: Aerodynamic Testing and Structural Dynamics. Interline Publishing Private Limited, B, pp. 1-19. ISBN 81-7296-040-9

Balasubramaniam, R and Somashekar, BR (1994) Ground vibration studies of aerospace structures- NAL's contribution. In: Aerodynamic Testing and Structural Dynamics. Interline Publishing Private Limited, Bangalore, pp. 1-15.

Prathap, Gangan and Naganarayana, BP and Somashekar, BR and Sudhakar, B (1992) Development of General Purpose Finite Element Package for Structural Analysis of Isotropic, Anisotropic and Layered13; Composite Structures: Progress Report. Technical Report. National Aerospace Laboratories, Bangalore, India.

Joshi, A and Somashekar, BR (1988) Effect of initial curvature on the panel flutter. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Rajagopal, P and Vijaya vittala, NG and Somashekar, BR (1988) Aeroelastic tailoring of unswept and forward swept advanced composite wings for divergence costraints. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Prathap, Gangan and Somashekar, BR (1988) A field-consistent 8-noded laminated anisotropic plate element. In: Proceedings of the International Conference on Composite materials and structures, 6-9 Jan 1988, Madras, India.

Prathap, Gangan and Somashekar, BR (1988) FIELD- AND EDGE-CONSISTENCY SYNTHESIS OF A 4-NODE QUADRILATERAL PLATE BENDING ELEMENT. International Journal for Numerical Methods in Engineering, 26 (8). pp. 1693-1708.

Prathap, Gangan and Naganarayana, BP and Somashekar, BR (1988) Field-consistency analysis of the isoparametric eight-noded plate bending element. Computers and Structures, 29 (5). pp. 857-873. ISSN 0045-7949

Prathap, Gangan and Somashekar, BR (1987) Field and edge consistency synthesis of a 4-Noded quadrilateral plate bending element. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Radhakrishna, BS and Ramani, TS and Somashekar, BR (1987) Use of postprocessor femview to interactively view structural displacements. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Somashekar, BR and Prathap, Gangan and Ramesh Babu, C. (1987) A Field-consistent, four-noded, laminated anisotropic plate/ shell element. Computers and Structures, 25 (3). pp. 345-353. ISSN 0045-7949

Somashekar, BR and Prathap, Gangan (1986) A Field-consistency error model for the single element test for the eight noded brick element. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Somashekar, BR (1986) A field-consistent 8-noded laminated anisotropic plate element. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Ramesh Babu, C and Somashekar, BR (1986) Single element test for aspect ratio sensitivity of solids - A field consistency error model. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Joshi, A and Somashekar, BR (1986) Effect of static inplane loads and boundary conditions on the flutter of flat rectangular panels. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Joshi, A and Somashekar, BR (1986) Effect of static inplane loads and boundary conditions on the flutter of flat rectangular panels. Journal of Aeronautical Society of India, 38 . pp. 105-112.

Aruna, HM and Guruprasad, K and Somashekar, BR (1985) Finite element modelling and analysis of a composite rudder. In: Conference on Finite Elements in Computational Mechanics, 2-6 Dec 1985, Bombay, India.

Somashekar, BR and Prathap, Gangan and Ramesh Babu, C (1985) A field-consistent 4-Noded laminated anisotropic plate/shell element. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Balasubramaniam, R and Somashekar, BR (1985) Direct digital test system for vibration studies of aircraft structures. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Somashekar, BR and Prathap, Gangan and Ramesh Babu, C (1985) ASKA and constrained multi-strain-field problems. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Ramesh Babu, C and Somashekar, BR and Prathap, Gangan (1985) Development of a library of field-consistent finite elements. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Upadhya, AR and Somashekar, BR (1984) Review of Launch Vehicle Related Aeroelastic Instability Studies at HAL. In: Analysis of Structures - A Commemorative volume published on the occasion of the 60th Anniversary of Dr. S.R.Valluri, Dec 1984, NAL, Bangalore, India.

Somashekar, BR and Ram, Nanjunda CS (1984) Analysis of swept plates with structural reduction using transition element concept. Computers and Structures, 18 (3). pp. 409-416. ISSN 0045-7949

Somashekar, BR and Nanjunda Ram, CS (1984) Non-dimensional design data for cantilever swept plates. Institution of Engineers, 64 . pp. 193-198.

Somashekar, BR and Prathap, Gangan (1983) Stress singularities in swept cantilever plates. Aeronautical Society of India, Journal, 35 . pp. 107-111. ISSN 0001-9267

Somashekar, BR and Krishnamurthy, AV and Ram, Nanjunda CS (1983) Study of swept cantilever wings employing inter-phase element concept for structural reduction. Aeronautical Society of India, Journal, 35 . pp. 77-105. ISSN 0001-9267

Somashekar, BR (1983) A simple selectively integrated torsion-flexure coupled tapered beam element with transverse shear deformation. Computers and Structures, 17 (3). pp. 403-406. ISSN 0045-7949

Somashekar, BR (1974) Application of digital computers in vibration testing and analysis. In: Seminar on the Role of Computers in Structural Analysis, Design and Optimisation, 13-14 June 1974, Bangalore, India.

Somashekar, BR (1971) The effect of aerodynamic lag on the bending response of wings at supersong speeds. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Kariappa, - and Somashekar, BR and Shah, CG (1970) Discrete element approach to flutter of skew panels with13; in-plane forces under yawed supersonic flow. AIAA Journal, 8 (11). pp. 2017-2022.

Kariappa, V and Somashekar, BR (1970) Flutter of skew panels by the matrix displacement approach. The Aeronautical Journal of the Royal Aeronautical Society, 74 (716). pp. 672-675.

Kariappa, - and Somashekar, BR (1965) Application of matrix displacement methods in the study of panel flutter. Technical Report. National Aeronautical Laboratory, Bangalore, India.

This list was generated on Thu Nov 27 04:17:54 2014 IST.