Fuselages were bodies of revolution with maximum diameters equal to 12% of fuselage length; nose shapes were circular, elliptical, and pointed; tests conducted for various angles of attack up to 30°; theoretical estimates of interference effect for zero angle of attack also included.
Investigation of fuselage interference on pitot-static tube extending forward from nose of fuselage
Nat Advisory Committee Aeronautics -- Tech Note
1947
21 pages
Article (Journal)
English
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