Analysis of damages on the compressor blades of an aircraft

Madan, M and Bhuvana, R and Sujata, M and Venkataswamy, MA and Bhaumik, SK (2011) Analysis of damages on the compressor blades of an aircraft. Project Report. National Aerospace Laboratories, Bangalore, India.

Full text not available from this repository. (Request a copy)

Abstract

Damages on the airfoil surface of compressor blades of an aircraft were analyzed. Analysis shows that the damages were caused due to impact of foreign object on the concave surface of the airfoil and hence, referred to as Foreign Object Damage (FOD). The nature of FOD suggests that the blade was most probably hit by a feathery, soft, solid mass. There were no evidences to suggest that the FOD was caused by either metallic object or stones/pebbles.

Item Type: Proj.Doc/Technical Report (Project Report)
Uncontrolled Keywords: Aircraft;Compressor blades;FOD
Subjects: AERONAUTICS > Aeronautics (General)
CHEMISTRY AND MATERIALS > Chemistry and Materials (General)
Division/Department: Materials Science Division, Materials Science Division, Materials Science Division, Materials Science Division, Materials Science Division
Depositing User: Ms. Alphones Mary
Date Deposited: 18 Jul 2011 10:32
Last Modified: 18 Jul 2011 10:32
URI: http://nal-ir.nal.res.in/id/eprint/9410

Actions (login required)

View Item