Aeronautical Engineering/Propeller Pitch

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Question
Dear Mr. Soderman,
    I have s quick question about propeller pitch and how it affects performance and efficiency.  Basically, does a lower angle equal more RPM or does a higher angle equal more RPM?  Thanks for your time!

Answer
On most aircraft pitch and rpm are independent variables, so I don't quite understand your question.  Do you mean - how can I recover the same thrust if pitch is reduced.  If so, the answer is to increase rpm unless you are reaching a limit.  Do you mean - what happens if I reduce the pitch on a constant HP engine. If so, the rpm will go up because there is less load on the engine.  Check the following website on propeller performance:

http://www.epi-eng.com/propeller_technology/selecting_a_propeller.htm

or write back with clarification.
Paul

Aeronautical Engineering

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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)

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