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Featured researches published by P.P. Sinha.


Materials Performance and Characterization | 2017

Anisotropy in Residual Stress Measurements in Aluminum Alloys Used in the Aerospace Industry

P. Ramesh Narayanan; Satyam Suwas; P.P. Sinha; S. Ranganathan

The aerospace industry has encountered many failures of the metallic hardware and sub-systems made of aluminum alloys, wherein the residual stresses are known to play a major role. This requires an accurate measurement of the residual stresses at various locations of the component in a nondestructive manner. The X-ray diffraction (XRD) method of measuring the residual stresses offers one of the most commonly used nondestructive techniques providing accurate stress values. The aluminum alloys, used for launch vehicle and satellite applications, are subjected to a variety of processing operations to realize the final product. These processes invariably introduce crystallographic texture in the material, which, in turn, influences the residual stresses measured using the diffraction method. The sin2ψ–2θ plots show nonlinearity in the longitudinal and transverse direction for the alloys studied. This nonlinearity could be caused by two major factors, namely, the crystallographic texture and stress gradient from the surface to the core of the sheets. In the case of aluminum alloys studied, both the factors play important roles by influencing the residual stress measurements. This paper covers the anisotropy in residual stress measurements caused by the influence of texture using the diffraction technique. Experiences at the Vikram Sarabhai Space Centre (VSSC) have been discussed with case studies on textured aluminum-alloy materials.


Engineering Failure Analysis | 2010

Failure analysis of titanium alloy (Ti6Al4V) fastener used in aerospace application

Abhay K. Jha; Satish Kumar Singh; M. Swathi Kiranmayee; K. Sreekumar; P.P. Sinha


Engineering Failure Analysis | 2009

High strain rate deformation and cracking of AA 2219 aluminium alloy welded propellant tank

Abhay K. Jha; S.V.S.N. Murty; K. Sreekumar; P.P. Sinha


Engineering Failure Analysis | 2010

Role of electro-discharge machining on the fatigue performance of 15–5PH stainless steel component

Abhay K. Jha; K. Sreekumar; P.P. Sinha


Engineering Failure Analysis | 2010

Cracking of Al–4.5Zn–1.5Mg aluminium alloy propellant tank – A metallurgical investigation

Abhay K. Jha; P. Ramesh Narayanan; K. Sreekumar; P.P. Sinha


Journal of Failure Analysis and Prevention | 2009

Cracking of Al–Zn–Mg Aluminum Alloy Nozzle Weld of Propellant Storage Tank: A Metallurgical Investigation

Abhay K. Jha; K. Sreekumar; P.P. Sinha


Engineering Failure Analysis | 2011

Failure analysis of M250 maraging steel stud used in Flex Nozzle Control actuator bracket of solid propulsion system

Abhay K. Jha; M. Swathi Kiranmayee; K. Sreekumar; P.P. Sinha


Journal of Manufacturing Processes | 2010

Process optimization for high fracture toughness of maraging steel rings formed by mandrel forging

Abhay K. Jha; K. Sreekumar; Thomas Tharian; P.P. Sinha


Engineering Failure Analysis | 2010

Metallurgical failure analysis of the 560 mm dia 0.15C–1.25Cr–1Mo–0.25V steel pressure vessel

Abhay K. Jha; K. Sreekumar; P.P. Sinha


Journal of Failure Analysis and Prevention | 2011

Cracking of Aluminum Alloy Rivets Used in Space Application: A Metallurgical Investigation

Abhay K. Jha; K. Sreekumar; P.P. Sinha

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Abhay K. Jha

Indian Space Research Organisation

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K. Sreekumar

Indian Space Research Organisation

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M. Swathi Kiranmayee

Indian Space Research Organisation

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P. Ramesh Narayanan

Indian Space Research Organisation

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M.C. Mittal

Indian Space Research Organisation

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S. Ranganathan

Indian Institute of Science

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S.V.S.N. Murty

Indian Space Research Organisation

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Satish Kumar Singh

Indian Space Research Organisation

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Satyam Suwas

Indian Institute of Science

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Sushant K. Manwatkar

Indian Space Research Organisation

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