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- W273130821 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." @default.
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- W273130821 date "1953-06-22" @default.
- W273130821 modified "2023-09-27" @default.
- W273130821 title "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" @default.
- W273130821 hasPublicationYear "1953" @default.
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