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Akademický článek
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Publikováno v:
Powder Technology. 394:1186-1194
Direct impingement (DI) erosion testing of steel and cobalt-based alloys is conducted with particles entrained in air and water. The tests are performed using 75- and 300-μm silica particles with three particle velocities and five impact angles. The
Publikováno v:
Concurrent Engineering. 16:139-147
This study presents an application of a distributed service-oriented architecture (FIPER) for the preliminary design of gas turbines. The FIPER architecture is based on the concept of registration and discovery of services in real time. It uses a ser
Publikováno v:
Engineering Optimization. 34:175-194
A multidisciplinary optimization procedure for gas turbine blade design has been developed and demonstrated on a generic 3-D blade. The blade is cooled both internally and externally (film cooling). Aerodynamic and heat transfer design criteria are i
Publikováno v:
Inverse Problems in Engineering. 8:283-308
A multidisciplinary optimization procedure for gas turbine airfoil design has been developed and demonstrated on a generic blade. Aerodynamic and heat transfer design objectives are integrated along with various constraints on the airfoil geometry. H
Publikováno v:
Mathematical Problems in Engineering, Vol 5, Iss 2, Pp 97-119 (1999)
Design optimization of a gas turbine blade geometry for effective film cooling toreduce the blade temperature has been done using a multiobjective optimization formulation. Three optimization formulations have been used. In the first, the average bla
A Robust & Secure System for Performing Engineering Analysis and Design in a Distributed Environment
Publikováno v:
45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference.
In today's fast paced economy product design is becoming increasingly complex and requires tighter integration of the engineering and business processes not only within the individual businesses, but also across enterprises. This high demand for real
Akademický článek
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Publikováno v:
8th Symposium on Multidisciplinary Analysis and Optimization.
A multidisciplin ary design optimization procedure for gas turbine blade design has been developed and demonstrated on a generic 3-D blade. Aerodynamic, heat transfer, structural and modal design objectives are integrated along with various constrain
Publikováno v:
41st Structures, Structural Dynamics, and Materials Conference and Exhibit.