Zobrazeno 1 - 10
of 21
pro vyhledávání: '"A.E. Muthunayagam"'
Publikováno v:
Desalination. 180:25-32
The feasibility of desalination by low pressure vaporization of seawater at temperatures between 26°C and 32°C was demonstrated in a pilot plant. The plant operated at vacuum pressures between 1.3 KPa and 2.3 KPa. The saline water was sprayed into
Publikováno v:
Applied Thermal Engineering. 25:941-952
A vapor diffusion model, which takes into account the reduction of droplet temperature during the evaporation process, was used to determine the achievable targets for desalination of seawater at temperatures between 26 °C and 32 °C when the saline
Autor:
K. Mohan Ram, A.E. Muthunayagam, Monalisha Nayak, Sangeneni Mohan, K. Rajanna, N. Gunasekaran
Publikováno v:
IEEE Transactions on Instrumentation and Measurement. 45:335-339
A differential pressure transducer with sputtered gold films as strain gauges has been designed and fabricated. The construction details of the sensing element assembly are given. The details of the strain gauge film configuration employed and the th
Publikováno v:
Measurement Science and Technology. 4:1319-1322
A diaphragm-type pressure transducer with a sputtered platinum film strain gauge (sensing film) has been designed and fabricated. The various steps followed to prepare thin film strain gauges on the diaphragm are described. M-bond 450 adhesive (Measu
Publikováno v:
Acta Astronautica. 26:779-798
Present day 1.8 tonne class geosynchronous satellites carry on-board the unified bipropellant propulsion system for apogee manoeuvre, attitude and orbit control and station keeping applications. Basically the mass is expelled from the satellite for t
Publikováno v:
IndraStra Global.
The behavior of a pressure transducer with Au-Ni (89:11) film as strain gauges have been studied. The effects of post-deposition heat treatment on the resistance of the thin-film strain gauges and hence the output performance of the pressure transduc
Publikováno v:
Journal of Materials Science Letters. 12
Publikováno v:
Acta Astronautica. 19:681-697
Solid rocket motors have been the mainstay of ISRO's sounding rockets and the first generation satellite launch vehicles. For the new launch vehicle under development also, the solid rocket motors contribute significantly to the vehicle's total propu
Autor:
A.E. Muthunayagam, K. Mastanaiah
Publikováno v:
AIAA Journal. 13:954-956
Akademický článek
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