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

Jacobs, Eastman N Ward, Kenneth E
naca-report-540
1936


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:
http://naca.central.cranfield.ac.uk/reports/1936/naca-report-540.pdf