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Advanced turboprop installation aerodynamicsThe expected aerodynamic effects of a propfan installed on a thick supercritical wing are summarized qualitatively. Nacelle/wing and jet interactions, slipstream incremental velocity, nonuniform inflow, and swirl loss recovery are discussed.
Document ID
19810010487
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Smith, R. C. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 11, 2013
Publication Date
February 1, 1981
Publication Information
Publication: NASA. Langley Research Center Advan. Aerodyn. and Active Controls
Subject Category
Aircraft Propulsion And Power
Accession Number
81N19013
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19810010475Collected WorksAdvanced aerodynamics and active controls. Selected NASA research
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