[b]SOME ASPECTS OF PROTECTION AGAINST CORROSION FOR THE GAS TURBINE STATOR[/b]
Journal Title: INCAS BULLETIN - Year 2011, Vol 3, Issue 1
Abstract
This paper continues the recent research of the author, considering the demands for turbines components. The turbine’s destinations are taken into consideration during the design phase, but the technological, architectural requirements as well as the ones regarding the materials they are made of, set the limits for the turbine design. The main determiner is the temperature.
Authors and Affiliations
Sorin PAVEL
VLM Tool for IDS Integration
This paper is dedicated to a very specific type of analysis tool (VLM - Vortex Lattice Method) to be integrated in a IDS - Integrated Design System, tailored for the usage of small aircraft industry. The major interest i...
Analysis of modern military jet trainer aircraft
New technical solutions and the application of modern technologies have led to combat aircraft configurations with a significant improvement in reliability, flight performance and operational performance through the crea...
Comprehensive study of endurance for IAR-99 Hawk
The paper presents some methods of on-ground and in-flight calibration for strain gauges, intended to the development of complex programs which analyze the endurance phenomena for aerospace structures, with direct applic...
Dynamic study of the virtual prototype of the IAR-99 SOIM Aircraft
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Automation of the inner design of the aircraft
The task of forming the wind-swept surface according to the results of the aircraft’s inner design is described. The approach of the integration of natural and virtual prototyping in the design of equipment compartments...