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Rotary balance data and analysis for the X-29A airplane for an angle-of-attack range of 0 deg to 90 degThe rotational aerodynamic characteristics are discussed for a 1/8 scale model of the X-29A airplane. The effects of rotation on the aerodynamics of the basic model were determined, as well as the influence of airplane components, various control deflections, and several forebody modifications. These data were measured using a rotary balance, over an angle of attack range of 0 to 90 deg, for clockwise and counter clockwise rotations covering an omega b/2V range of 0 to 0.4.
Document ID
19870001404
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ralston, J. N. (Bihrle Applied Research, Inc. Jericho, NY, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1984
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-3747
NAS 1.26:3747
Accession Number
87N10837
Funding Number(s)
PROJECT: RTOP 505-43-13-01
CONTRACT_GRANT: NAS1-16205
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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