Interference of wing and fuselage from tests of 209 combinations in the NACA variable-density tunnel

Jacobs, Eastman N Ward, Kenneth E

This report presents the results of tests of 209 simple wing-fuselage combinations made in the NACA variable-density wind tunnel to provide information regarding the effects of aerodynamic interference between wings and fuselages at a large value of Reynolds number.

An Adobe Acrobat (PDF) file of the entire report: