Damage Resistance of a Thermal Barrier Coated Superalloy used in Aero Turbine Blade under Accelerated Creep Condition
Main Authors: | Ray, A. K., Krishna, G., Swaminathan, J., Bose, S.C., Roy, N., Tiwari, Y.N., Roy, P.K., Alam, Z., Sharma, V.S.R.A., Venkatraman, B., Das, D.K. |
---|---|
Format: | Article |
Language: | English |
Published: |
De Gruyter
2009-04-01
|
Series: | High Temperature Materials and Processes |
Online Access: | https://doi.org/10.1515/HTMP.2009.28.1-2.35 |
Similar Items
-
High Temperature Mechanical Properties of Thermal Barrier Coated Superalloy Applied to Combustor Liner of Aero Engines
by: Ray, A.K., et al.
Published: (2006-06-01) -
Numerical modelling of creep deformation in a CMSX-4 single crystal superalloy turbine blade
by: Dye, D, et al.
Published: (2008) -
Aero-Elastic Stability of Horizontal Axis Wind Turbine Blades
by: Seyyed A. Sina
Published: (2021-07-01) -
Fatigue Failure in High-Temperature Single Crystal Superalloy Turbine Blades
by: Arakere, Nagaraj K., et al.
Published: (2001-05-01) -
Aero-thermal performance of transonic high-pressure turbine blade tips
by: O'Dowd, D
Published: (2010)