Aeronautical Engineering/fan blade geometry

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Question
i am a a-level physics student trying to calculate the likely stress in a turbine blade of a Jet engine under normal operating conditions. in order to do this i have trying to find information about the geometry of turbine fan blades so that i could work out the mass of a single blade which together with its speed of rotation would enable me to calculate the stress it experiences, any help with this would be much appreciated.

Thank you very much

yours in anticipation

Bob

Answer
Bob
As you can imagine there are big turbofans and small turbofans.  Here is a link to the GE J85 turbojet:

http://en.wikipedia.org/wiki/General_Electric_J85

It is on the smaller size, but you can scale off the turbine blade dimensions from the specifications and the image of the cut away engine.  True dimensions are hard to find.  The turbine blades are curved rectangles with some camber more or less.  It is a two-stage turbine.
Paul

Aeronautical Engineering

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Paul Soderman

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Aeronautics, Fluid Mechanics, Aeroacoustics, Noise Control, Muffler Design, Wind Tunnel Research.... I know nothing about India - do not ask about schools, jobs, application requirements, career choices, etc. for India. Please, no text message verbiage; I prefer full words in full sentences. Thanks.

Experience

38 years as research engineer at NASA

Publications
AIAA, NASA

Education/Credentials
B.S. and M.S. Aeronautical Engineering - U. of Washington Graduate work Standford U.

Awards and Honors
AIAA Associate Fellow (American Institute of Aeronautics and Astronautics)

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