Interaction Between Air Propellers and Airplane Structures (1927)
NASA Technical Reports Server (NTRS) · leaf 8
sity. (Fuselage shortened lo accommodate dynamometer) derant degree be due to the nose of the fuselage rather than to the wings and tail surfaces. The nose of the model was fitted with a. wire mesh, 40 spaces per inch, and wire 0.000 inch diameter. This is found to have an air resistance closely… … falling off of influence on the FIG, ().—Model c propeller with increase of distance between the propeller and the obstructing surface or body. These results all tend to support definitely the conclusion that the influence of surfaces giving generally a frictional drag and at distances of one and…
NASA Technical Reports Server (NTRS)
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