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About Paul Soderman
Expertise
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)

 
   

You are here:  Experts > Science > Aerospace/Aviation > Aeronautical Engineering > propeller with steel deflectors

Aeronautical Engineering - propeller with steel deflectors


Expert: Paul Soderman - 9/2/2009

Question
I need help beginning my research on the effects of using steel deflectors on a farmer propeller when its the triangular shape as used by Roland Gaross. Can you please tell me how this would effect the flow of air around the propeller and how it can effect the plane's capability on pitch and yawing. If you can please refer me to a book or website that can help me study the subject better because I am writing a paper comparing the Fokker E III and the Morane-Saulnier Type L with steel deflectors in terms of maneuverability. Thank You

Answer
Terri
You haven't told me what the steel deflectors looked like.  In general, adding anything with significant thickness to a propeller would compromise the performance of the propeller.  One thing in Gaross's favor was that the steel deflectors must have been put on the airfoil lower surface, which is less critical than the upper surface.  But changing the airfoil shape is not good and could reduce thrust and increase torque required due to drag increase.  The other factor is the mass of the deflectors which would have added angular momentum to the propeller.  That would make it harder to maneuver a light aircraft just as moving a gyroscope is resisted by the angular momentum of the spinning mass and introduces new forces.  In other words, a command to pitch the aircraft would introduce a force and moment in another direction. These things can be computed.

I don't know what book might help except a basic physics or dynamics book that would describe the forces and moments on a spinning body.  Do a Google search on gyroscope. Likewise, propeller performance charts may give a clue as to how airfoil shape changes propeller performance, but if it was a simple protuberance it might be difficult to find data that matches.
Paul

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