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Analysis of compressor stage I rotor blades of an aeroengine

IR@NAL: CSIR-National Aerospace Laboratories, Bangalore

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Title Analysis of compressor stage I rotor blades of an aeroengine
 
Creator Madan, M
Venkataswamy, MA
Sujata, M
Bhaumik, SK
 
Subject Aeronautics (General)
Chemistry and Materials (General)
 
Description Two compressor stage I blades from an aeroengine were analyzed. Though some faint linear indications were observed on the airfoil surface of the blades on FPI, SEM examination revealed that these were due to externally deposited materials on the airfoil surface. SEM examination did not reveal any cracks in the blades.
 
Publisher National Aerospace Laboratories
 
Date 2007
 
Type Proj.Doc/Technical Report
NonPeerReviewed
 
Identifier Madan, M and Venkataswamy, MA and Sujata, M and Bhaumik, SK (2007) Analysis of compressor stage I rotor blades of an aeroengine. Project Report. National Aerospace Laboratories, Bangalore, India.
 
Relation http://nal-ir.nal.res.in/9547/