Analytical determination of propeller performance degradation due to ice accretion /

Analytical determination of propeller performance degradation due to ice accretion /

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"A computer code has been developed which is capable of computing propeller performance for clean, glaze, or rime iced propeller configurations, thereby providing a mechanism for determining the degree of performance degradation which results from a given icing encounter. The inviscid, incompr...

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Bibliographic Details
Main Author: Miller, Thomas L.
Corporate Authors: Sverdrup Technology, Inc, Lewis Research Center, United States. National Aeronautics and Space Administration
Format: Government Document Microform Book
Language:English
Published: Cleveland, Ohio : Sverdrup Technology, Inc. : Lewis Research Center, [1986]
Series:NASA contractor report ; NASA CR-175092.
Subjects:
Propellers, Aerial > Aerodynamics > Testing > Computer programs.
Icing (Meteorology) > Computer programs.
Degradation.
Ice formation.
Incompressible flow.
Inviscid flow.
Propellers.
Propellers - Airfoils - Ice formation - Degradation - Thrust - Torque - Incompressible flow - Inviscid flow - Computer programs - Correlation - Specifications

Evans: US Documents Microfiche (3rd floor)

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Call Number: NAS 1.26:175092