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Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 20 to 90 deg. 3: Influence of control deflection on predicted model D spin modesThe influence of control deflections on the rotational flow aerodynamics and on predicted spin modes is discussed for a 1/6-scale general aviation airplane model. The model was tested for various control settings at both zero and ten degree sideslip angles. Data were measured, using a rotary balance, over an angle-of-attack range of 30 deg to 90 deg, and for clockwise and counter-clockwise rotations covering an omegab/2V range of 0 to 0.5.
Document ID
19840017573
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ralston, J. N. (Bihrle Applied Research, Inc. Jericho, NY, United States)
Barnhart, B. P. (Bihrle Applied Research, Inc. Jericho, NY, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1984
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:3248
NASA-CR-3248
Accession Number
84N25641
Funding Number(s)
CONTRACT_GRANT: NAS1-16205
PROJECT: RTOP 505-43-13-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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