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Number of items: 15.

Dash, PK (2006) Can We Hope to Make Today's Concern about Ageing Aircraft - a Thing of the Past? In: Proceedings of 14th National Seminar on Aerospace Structures: Fatigue, Fracture and Ageing Structures, 30-31 Jan 2006, Nagpur, India.

Manjunatha, CM (2006) Fatigue crack growth prediction under spectrum load using crack driving force DK 13;. AIAA Journal, 44 (2). pp. 396-399. ISSN 0001-1452

Manjunatha, CM and Chandra, Anil AR and Ranganath, VR (2006) Fatigue crack growth prediction under Falstaff load sequence by K*-RMS approach. In: International Seminar on Fatigue, Fracture and Durability, 26-28 Jun 2006, IISc., Bangalore.

Manjunatha, CM and Chandra, Anil AR and Ranganath, VR (2006) Modification of falstaff load sequence to accelerate fatigue tests. In: Proceedings of the National Conference on Mechanical Engineering (NATCON.ME-2006), 26-27 May 2006, Tumkur, India.

Manjunatha, CM and Chandra, Anil AR and Ranganath, VR (2006) New procedure for crack growth prediction under spectrum loads. In: ATM 2006, 15-16 Nov 2006, Jamshedpur, India.

Manjunatha, CM and Ranganath, VR (2006) Effect of Airframe Materials on Spectrum Modification for Full Scale Fatigue Testing sf an Ageing Aircraft. In: Proceedings of the 14th National Seminar on Aerospace Structures: Fatigue, Fracture and Ageing Structures, 30-31 Jan 2006, Nagpur, India.

Manjunatha, CM and Ranganath, VR (2006) Spectrum Modification for Full Scale Fatigue Testing of an Ageing Aircraft. In: Proceedings of 14th National Seminar on Aerospace Structures: Fatigue, Fracture and Ageing Structures, 30-31 Jan 2006, Nagpur, India.

Manjunatha, CM and Ranganath, VR and Sujatha, S and Sureshkumar, M and Venkataswamy, M (2006) Estimation of service load sequence from fatigue fracture surface analysis (Paper No. DD-5). In: National Conference on Failure Analysis, NCFA-2006, 22-23 Dec 2006, Hyderabad, India.

Ray, AK and Roy, N and Dash, B and Das, DK and Ranganath, VR (2006) High temperature mechanical properties of thermal barrier coated superalloy applied to combustor liner of aero engines13;. High Temperature Materials and Processes, 25 (1-2). pp. 109-121.

Sahoo, PK and Dattaguru, B and Murthy, CRL (2006) Finite Element Analysis of Adhesively Bonded Lap Joints. In: Proceedings of the 14th National Seminar on Aersopace Structures: Fatigue, Fracture and Ageing Structures, 30-31 Jan 2006, Nagpur, India.

Singh, KL (2006) Analysis of Flight Parameters to Derive Load Spectrum Sequence for Full Scale Fatigue Testing of an Ageing Aircraft. In: Proceedings of the 14th National Seminar on Aerospace Structures: Fatigue, Fracture and Ageing Structures, 30-31 Jan 2006, Nagpur, India.

Singh, KL and Dattaguru, B and Ramamurthy, TS (2006) Numerically integrated MVCCI for fracture analysis on delaminated composite panels in compression. Mechanics of Advanced Materials and Structures, 13 (4). pp. 303-316.

Singh, KL and Manjunatha, CM and Venkata, NM (2006) Modeling and stress analysis of stiffened carbon fiber composite panels. In: Proceedings of National Seminar on Composites INCCOM-5, ISAMPE, 24-25 Nov 2006, Hyderabad, India.

Sivaprasad, S and Tarafder, S and Ranganath, VR and Tarafder, M and Ray, KK (2006) Corrosion fatigue crack growth behaviour of naval steels. Corrosion Science, 48 (8). pp. 1996-2013.

Suresh Kumar, M and Madan, M and Venkataswamy, MA and Manjunatha, CM and Ranganath, VR and Sujata, M and Bhaumik, SK (2006) Failure analysis of compressor rotor blades of 500 MW generator. Project Report. National Aerospace Laboratories, Bangalore, India.

This list was generated on Wed Jul 30 01:22:06 2014 IST.