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Arrangement of Fusiform Bodies to Reduce the Wave Drag at Supersonic Speeds

出版	National Advisory Committee for Aeronautics, 1954
URL	http://books.google.com.hk/books?id=sR7JSgAACAAJ&hl=&source=gbs_api

註釋Using linearized slender-body theory and reverse-flow theorems, the wave drag of a system of fusiform bodies at zero angle of attack and supersonic speeds is studied to determine the effect of varying the relative location of the component parts. The investigation is limited to two-body and three-body arrangements of Sears-Haack minimum-drag bodies. It is found that in certain arrangements the interference effects are beneficial, and may even result in the two- or three body system having no more wave drag than that of the principal body alone. The most favorable location appears to be one in which the maximum cross section of the auxiliary body is slightly forward of the Mach cone from the tail of the main body. The least favorable is the region between the Mach cone from the nose and the forecone from the tail of the main body.