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Aerodynamic problems in the design of efficient propellers

Lewis Feldman

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Abstract

From General Analysis: The purpose of part I of this paper is to show how the loading that gives the minimum induced energy loss can be obtained from rather elementary considerations and to present design charts from which such a plan form can be quickly obtained for any set of design conditions.

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From General Analysis: The purpose of part I of this paper is to show how the loading that gives the minimum induced energy loss can be obtained from rather elementary considerations and to present design charts from which such a plan form can be quickly obtained for any set of design conditions.

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Available abstract

From General Analysis: The purpose of part I of this paper is to show how the loading that gives the minimum induced energy loss can be obtained from rather elementary considerations and to present design charts from which such a plan form can be quickly obtained for any set of design conditions.

Key concepts: Aerodynamics, Set (abstract data type), Plan (archaeology), Computer science, Engineering, Aerospace engineering, Geology, Programming language

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