Revistas
Artículos
Publicaciones
Documentos
REVISTA
JOURNAL OF TURBOMACHINERY
TODAS
Inicio
/
JOURNAL OF TURBOMACHINERY
/
Vol: 123 Núm: 4 Par: 0 (2001)
/
Artículo
ARTÍCULO
TITULO
Turbine Nozzle Endwall Film Cooling Study Using Pressure-Sensitive Paint
Luzeng J. Zhang and Ruchira Sharma Jaiswal
Resumen
No disponible
PÁGINAS
pp. 730 - 738
NÚMERO
Volumen: 123 Número: 4 Parte: 0 (2001)
MATERIAS
INGENIERÍA Y CONSTRUCCIÓN CIVIL
REVISTAS SIMILARES
Aerospace
Applied Sciences
Applied and Computational Mechanics
Artículos similares
Clocking and Potential Effects in Combustor?Turbine Stator Interactions
Acceso
Pawel Flaszynski, Michal Piotrowicz and Tommaso Bacci
Investigations of combustors and turbines separately have been carried out for years by research institutes and aircraft engine companies, but there are still many questions about the interaction effect. In this paper, a prediction of a turbine stator?s ...
ver más
Revista:
Aerospace
Monte Carlo Predictions of Aero-Engine Performance Degradation Due to Particle Ingestion
Acceso
Matthew Ellis, Nicholas Bojdo, Antonio Filippone and Rory Clarkson
Aero-engines, which encounter clouds of airborne particulate, experience reduced performance due to the deposition of particles on their high-pressure turbine nozzle guide vanes. The rate of this degradation depends on particle properties, engine operati...
ver más
Revista:
Aerospace
Unsteady Flow Structures within a Turbine Rim Seal Cavity in the Presence of Purge Flow?An Experimental and Computational Unsteady Aerodynamics Investigation
Acceso
Cengiz Camci, Michael Averbach and Jason Town
Flow within the space between the rotor and stator of a turbine disk, and an area referred to as the rim seal cavity, develops azimuthal velocity component from the rotor disk. The fluid within develops unsteady structures that move at a fraction of the ...
ver más
Revista:
Aerospace
Aerodynamic loading acting on the stator vane in the variable nozzle turbine flow
Acceso
Miroslav ?atko
s-
Revista:
Applied and Computational Mechanics
The Effect of Combustor-Turbine Interface Gap Leakage on the Endwall Heat Transfer for a Nozzle Guide Vane
Acceso
S. P. Lynch and K. A. Thole
Revista:
JOURNAL OF TURBOMACHINERY
Revistas destacadas
Infrastructures
Informed Infraestructure
BiT
Revista de la Construcción
Ver todas las revistas