Radhakrishnan, S and Krishnan, RV and Ramachandran, V (1986) Damage to the Compressor Blades of Ajeet E-2021 Engine. Project Report. National Aerospace Laboratories, Bangalore.
A second stage stator blade and three sixth stage rotor blades were recovered from the wreckage of an aircraft accident. The stator blade had a nick and this damage was due to rubbing action of another object. Soot had deposited on the rotor blades but not in the regions where the blades were overlapping . This indicates that the deposition of soot should have occurred after the blades got bent, i.e, after the accident.
|Item Type:||Proj.Doc/Technical Report (Project Report)|
|Uncontrolled Keywords:||Stator;Rotor;Compressor blade damage|
|Subjects:||CHEMISTRY AND MATERIALS > Chemistry and Materials (General)|
|Division/Department:||Materials Science Division , Materials Science Division, Materials Science Division|
|Depositing User:||Smt Bhagya Rekha KA|
|Date Deposited:||08 Aug 2012 11:08|
|Last Modified:||08 Aug 2012 11:08|
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- Damage to the Compressor Blades of Ajeet E-2021 Engine. (deposited 08 Aug 2012 11:08)[Currently Displayed]
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