REVISTA

International Journal of Turbomachinery, Propulsion and Power

ISSN: 2504-186X Frecuencia: 4 Formato: Electrónica

Tablas de contenido

7 artículos asociados

Volumen 2 Número 0 Parte 2 Año 2017

Adjoint-Based Design Optimisation of an Internal Cooling Channel U-Bend for Minimised Pressure Losses	Acceso
Tom Verstraete, Lasse Müller and Jens-Dominik Müller

Effects of the Approximations Embodied in the Momentum Theory as Applied to the NREL PHASE VI Wind Turbine	Acceso
Rodolfo Bontempo and Marcello Manna

Linear Stability Prediction of Vortex Structures on High Pressure Turbine Blades	Acceso
Markus Zauner, Neil D. Sandham, Andrew P. S. Wheeler and Richard D. Sandberg

Analysis of the Aerodynamic and Structural Performance of a Cooling Fan with Morphing Blade	Acceso
Alessio Suman, Annalisa Fortini, Nicola Aldi, Michele Pinelli and Mattia Merlin

Hot Streak Evolution in an Axial HP Turbine Stage	Acceso
Paolo Gaetani and Giacomo Persico

On Initiation of Stall in Axial Flow Compressors	Acceso
Jerzy A. Owczarek

Transition Models for Turbomachinery Boundary Layer Flows: A Review	Acceso
Erik Dick and Slawomir Kubacki