Interference of Wing and Fuselage from Tests of 17 Combinations in the NACA Variable-density Tunnel Combination with Special Junctures
This is a 1938 NACA technical report by NASA's Technical Reports Server collection, testing wing and fuselage combinations in the NACA variable-density wind tunnel. Its charts plot lift, drag and pitching moment against angle of attack for 17 model configurations, and its photographs show wooden wing-fuselage models with loading-edge fillets, which a designer might use for studying streamlined aircraft form and junction shapes through clean line graphs and sleek model silhouettes.
