1953•NASA STI Repository (National Aeronautics and Space Administration)Requires access
The Effect of Nacelle Combinations and Size on the Zero-lift Drag of a 45 Degree Sweptback Wing and Body Configuration as Determined by Free-flight Tests at Mach Numbers Between 0.8 and 1.3
Sherwood Hoffman, W. PEPPER
Open publisher page 0 citations
Abstract
Investigation of the effect on zero-lift drag of varying the size and number of symmetrically mounted nacelles on a 45 degree sweptback wing and body combination as determined by free-flight tests of rocket-propelled models over a range of Mach and Reynolds numbers. The nacelle configuration consisted of a twin-engine nacelle near the fuselage, a combination of single-engine nacelles at the wing tip and fuselage, a large nacelle at the wing tip, and a large nacelle near the fuselage.