Research graph
References from Computational investigation of film cooling from cylindrical and row trenched cooling holes near the combustor endwall. Local targets link to admitted publications; unresolved targets remain external evidence.
Film cooling effectiveness for short film cooling holes fed by a narrow plenum
10.1115/1.1303705 · 2000 · External reference
Measurements of discharge coefficients in film cooling
10.1115/1.2841307 · 1999 · External reference
Flow field computations of combustor–turbine interactions relevant to a gas turbine engine
10.1115/1.1625691 · 2004 · External reference
Unresolved reference
2008 · External reference
10.11113/jt.v58.1540
10.11113/jt.v58.1540 · External reference
Dynamic analysis of flow field at the end of combustor simulator
10.11113/jt.v58.1540 · 2012 · External reference
Influence of flow structure on compound angled film cooling effectiveness and heat transfer
10.1115/1.4002420 · 2011 · External reference
Film cooling over a concave surface through two staggered rows of compound angle holes
10.1080/02533839.2005.9671053 · 2005 · External reference
Effect of trench width and depth on film cooling from cylindrical holes embedded in trenches
2009 · External reference
Experimental simulation of a film cooled turbine blade leading edge including thermal barrier coating effects
10.1115/1.4000537 · 2011 · External reference
Influence of leading-edge lateral injection angles on the film cooling effectiveness of a gas turbine blade
2004 · External reference
effect of coolant-mainstream blowing ratio on leading edge film cooling flow and heat transfer-LES investigation
10.1016/j.ijheatfluidflow.2008.02.007 · 2008 · External reference
Simulations of multiphase particle deposition on end wall film-cooling holes in transverse trenches
2012 · External reference
Experimental investigation on the effects of a large recirculating area on the performance of an effusion cooled combustor liner
10.1115/1.4004729 · 2012 · External reference
Bump and trench modifications to film-cooling holes at the vane-end wall junction
10.1115/1.2812933 · 2008 · External reference
Gas turbine engine durability impacts of high fuel-air ratio combustors: near wall reaction effects on film-cooled backward-facing step heat transfer
10.1115/1.2056532 · 2006 · External reference
Film cooling performance of converging slot-hole rows on a gas turbine blade
10.1016/j.ijheatmasstransfer.2010.07.036 · 2010 · External reference
Film cooling performance of converging-slot holes with different exit–entry area ratios
2011 · External reference
Effects of obstructions and surface roughness on film cooling effectiveness with and without a transverse trench
10.1115/1.2950063 · 2009 · External reference
Flow and thermal field measurements in a combustor simulator relevant to a gas turbine aero engine
10.1115/1.1806455 · 2005 · External reference
Film cooling enhancement with surface restructure [Ph.D. thesis]
2009 · External reference
Turbine airfoil net heat flux reduction with cylindrical holes embedded in a transverse trench
10.1115/1.2812967 · 2009 · External reference
Flow field simulations of a gas turbine combustor
10.1115/1.1475742 · 2002 · External reference