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Rotary balance data for a single engine general aviation design having a high aspect-ratio canard for an angle-of-attack range of 30 deg to 90 degAerodynamic characteristics obtained in a helical flow environment utilizing a rotary balance located in the Langley spin tunnel are presented in plotted form. The configurations tested included the basic airplane, various control deflections, two canard locations, and wing leading edge modifications, as well as airplane components.
Document ID
19810004511
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mulcay, W. J. (Bihrle Applied Research, Inc. Jericho, NY, United States)
Rose, R. (Bihrle Applied Research, Inc. Jericho, NY, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1980
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-3170
Accession Number
81N13022
Funding Number(s)
CONTRACT_GRANT: NAS1-14849
PROJECT: RTOP 505-41-13-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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