Publication Date:
2019-06-28
Description:
The 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.
Keywords:
AERODYNAMICS
Type:
NASA-CR-3248
,
NAS 1.26:3248
Format:
application/pdf
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