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Code Estimates Helicopter-Rotor Inflow And Wake VelocitiesDOWN computer program implements flat-wake theory, which provides simple analysis for calculation of inflow and wake velocities of helicopter rotors. Written in FORTRAN 77.
Document ID
19930000782
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Curtiss, Howard C. (Princeton Univ.)
Mckillip, Robert M. (Princeton Univ.)
Wilson, John C. (Army Aviation Systems Command)
Date Acquired
August 16, 2013
Publication Date
December 1, 1993
Publication Information
Publication: NASA Tech Briefs
Volume: 17
Issue: 12
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-14841
ISSN: 0145-319X
Report Number: LAR-14841
Accession Number
93B10782
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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