GasTurbnLab: a multidisciplinary problem solving environment for gas turbine engine design on a network of nonhomogeneous machines; Heat transfer coefficient on the squealer tip and near squealer tip regions of a gas...
Chromium reduction in gas turbine engines;Combustion in a Transonic Flow with Large Axial and Transverse Pressure Gradients;Computer-aided design of gating systems for gas turbine engine rotor blades;CONCEPTUAL AND...
[篇名] A Comparison of the Creep behaviour of the Single Crystal Blade Alloys CMSX-4 and CM186LC, [ 篇名 ] A simulating study on thermal efficiency of a small gas turbine engine with a reciprocating gasifier (Part Ⅱ)...