Amanote Research
Register
Sign In
Probabilistic Performance Analysis of Eroded Compressor Blades
doi 10.1115/pwr2005-50070
Full Text
Open PDF
Abstract
Available in
full text
Date
January 1, 2005
Authors
A. Kumar
P. B. Nair
A. J. Keane
S. Shahpar
Publisher
ASMEDC
Related search
An Investigation on Failure Analysis of Titanium Gas Turbine Compressor Blades
Materials Science Forum
Mechanics of Materials
Materials Science
Condensed Matter Physics
Mechanical Engineering
Experimental and Numerical Modal Analysis of the First and Second Stage Compressor Blades
Engineering Solid Mechanics
Mechanics of Materials
Alloys
Plastics
Civil
Polymers
Metals
Structural Engineering
Composites
Ceramics
Experimental Crack Propagation Analysis of the Compressor Blades Working in High Cycle Fatigue Condition
Fatigue of Aircraft Structures
Mechanics of Materials
Risk
Civil
Structural Engineering
Reliability
Safety
Quality
Aerospace Engineering
Geometric Modelling of S-Shaped Skeletal Lines Profile of Axial Compressor Blades
Herald of Aeroenginebuilding
Surface Layer Quality in Compressor Titanium Blades at Multiaxes Deep Grinding
Science intensive technologies in mechanical engineering
Uncertainty Analysis of Aerodynamic Performance for Tip Clearance Size of Compressor
Conceptual Study on the Stator Blades of the Axial Flow Compressor With ‘M’ Cut
International Journal of Engineering Applied Sciences and Technology
Performance Limits of Axial Compressor Stages
The Two Dimensional Inflow Conditions for a Supersonic Compressor With Curved Blades