ARTÍCULO
TITULO

Adiabatic Effectiveness Measurements and Predictions of Leakage Flows Along a Blade Endwall

W. W. Ranson    
K. A. Thole    
and F. J. Cunha    

Resumen

No disponible

 Artículos similares

       
 
Hui Tang, GeonHwan Cho, Mario Patinios, James A. Scobie, Carl M. Sangan, J. Michael Owen and Gary D. Lock    
Ingress is the penetration of a hot mainstream gas in a turbine annulus through the rim seal into the wheel-space between the rotating turbine disc (the rotor) and the adjacent stationary casing (the stator). Purge flow is used to prevent or reduce ingre... ver más
Revista: Aerospace

 
Wei Shi, Pingting Chen, Xueying Li, Jing Ren and Hongde Jiang    
The film cooling holes in the blade of modern gas turbines have commonly been manufactured by laser drilling, Electric Discharge Machining (EDM), and Additive Manufacturing (AM) in recent years. These manufacturing processes often result in small geometr... ver más
Revista: Aerospace

 
A. A. Thrift, K. A. Thole, and S. Hada    

 
Bruno Facchini, Lorenzo Tarchi, Lorenzo Toni and Alberto Ceccherini    

 
J. R. Christophel, E. Couch, K. A. Thole, and F. J. Cunha     Pág. 251 - 262