Browse by Department

Up a level
Export as [feed] RSS 2.0 [feed] RSS 1.0 [feed] Atom
Group by: Creators Name | Item Type | No Grouping
Jump to: B | G | J | L | M | N | P | R | S | V
Number of items: 32.

B

Balasubramaniam, R and Shankar, V and Ramakrishna, DS and Nagaraja, SV (1988) Ground Resonance studies of HS 748 (unmodified ) Aircraft. Project Report. National Aerospace Laboratories, Bangalore.

Balasubramanian, TS (1988) Dynamic analysis of MiG-21 rudder (Metallic and composite). Project Report. National Aerospace Laboratories, Bangalore.

Balasubramanian, TS (1988) Dynamic strain monitoring of a EE pod during environmental tests. Project Report. National Aerospace Laboratories, Bangalore.

Bapu Rao, MN and Ashok Kamath, . and Kundavi Rani, . (1988) Stress Analysis of Prithvi Missil Wing Subjected to Aerodynamic Forces. Project Report. National Aerospace Laboratories, Bangalore.

G

Guruprasad, K and Subba Rao, M and Chandra, Ramesh (1988) Finite element analysis of composite rudder for DO 228 Aircraft 13; 13;. In: Composite Materials and Structures, 6-9 Jan 1988, Madras, India.

J

Joshi, A (1988) Free vibration analysis of HS0748 L Theoretical study and comparison with test results. Project Report. National Aerospace Laboratories, Bangalore.

Joshi, A and Madhusudan, BS (1988) Free Vibration analysis of Rotodome - pylon assembly. Project Report. National Aerospace Laboratories, Bangalore.

Joshi, A and Madhusudhan, BS (1988) Free vibration analysis of Free vibration analysis of HS-748 integrated with pylone and deck plate. Project Report. National Aerospace Laboratories, Bangalore.

Joshi, A and Ramamurthy, MR (1988) Aeroelastic testing of PSLV models. Project Report. National Aerospace Laboratories, Bangalore.

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

L

Lakshminarayana, HV and Ramani, TS (1988) On improving the performance of a shear-flexible triangular laminated composite plate finite element. In: Proceedings of the International Conference on Composite materials and structures, 6-9 Jan 1988, Madras, India.

M

Madhava, MR and Sudheendra, HN and Sridhara, S and Ramachandra, HV (1988) NON- Destructive Evaluation of Mig 21 composite Rudder. Project Report. National Aerospace Laboratories, Bangalore.

Murthy, MVV and Bapu Rao, MN (1988) Three-Dimensional stress problem of a finite thick plate with a through crack under tension.13;. International Journal of Solids and Structures, 24 (7). pp. 693-703.

Murthy, MVV and Viswanath, S and Rao, krishna Murty (1988) Two-dimensional model for crack closure effect in plates under bending 13; 13;. Engineering Fracture Mechanics, 29 (4). pp. 435-452. ISSN 0013-7944

N

Naganarayana, BP and Prathap, Gangan (1988) Consistency aspects of out-of plane bending, torsion and shear in a quadratic curved beam element. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Naganarayana, BP and Prathap, Gangan (1988) Consistent force resultant distributions in a quadratic Cquot; beam element with varying sectional properties. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Naganarayana, BP and Prathap, Gangan (1988) Displacement and stress predictions from field-and line-consistent versions of the 8-node mindlin plate element13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Naganarayana, BP and Prathap, Gangan (1988) Implementation of 2-node Shear-flexible field-consistent13; composite beam element in SAP IV. Technical Report. National Aeronautical Laboratory, Bangalore, India.

P

Prathap, Gangan (1988) The variational basis for the least-squares field- redistribution of strainFunctions in the finite element formulation of constrained media elasticity. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Naganarayana, BP (1988) Analysis of locking and stress oscillations in a general curved beam element. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Naganarayana, BP (1988) Consistency and orthogonality requirements and accurate stress recovery from the assumed strain eight noded quadrilateral plate bending element. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Prathap, Gangan and Naganarayana, BP (1988) Field-consistency rules for a three-moded shear flexible beam element under non-uniform isoparametric mapping. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prathap, Gangan and Naganarayana, BP (1988) Field-consistency rules for a three-noded shear flexible beam element under non-uniform isoparametric mapping13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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 (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.

R

Rajagopal, P and Lakshminarayana, HV (1988) Application of Aeroelastic Tailoring in lifting surface design. Project Report. National Aerospace Laboratories, Bangalore.

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.

S

Sridhara, S and Nagesh, KS (1988) TRlELE: A finite element software for the analysis of laminated composite plates and shells. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Sridhara Murthy, S (1988) Static Analysis of rotodomed aircraft Part I Nastran Substructure Modelling. Project Report. National Aerospace Laboratories, Bangalore.

Sridhara Murthy, S and Viswanath, S and Gangan , .Prathap (1988) Static Analysis of Rotodomed aircraft Part II: Results for vertical gust load case (vB1). Project Report. National Aerospace Laboratories, Bangalore.

Structures, Division (1988) Dynamic analysisof HS 748 Modified for AEW Role a Proposal. Project Report. National Aerospace Laboratories, Bangalore.

V

Viswanathan, KS and Jayasurya, M and Subba Rao, M (1988) Fabrication of Composite parts of composite rudder for a typical military aircraft. Project Report. National Aerospace Laboratories, Bangalore.

This list was generated on Tue Jul 29 01:23:40 2014 IST.