A wind tunnel investigation of influence of a sting support with an angle-of-attack range of 110 deg to the model is described. The influence on the aerodynamic coefficients of a larger object in the detached region of downwash of a wing is discussed. The influence of the sting support is small in the whole angle-of-attack range. The influence of an object in the region of downwash of the wing can influence the aerodynamic coefficients.
Influence of a 90 Deg Sting Support on the Aerodynamic Coefficients of the Investigated Aircraft Model
1986
35 pages
Report
Keine Angabe
Englisch
Computation of Aerodynamic Coefficients for Transport Aircraft with MEGAFLOW
British Library Conference Proceedings | 2005
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