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- W1783371072 abstract "Report presenting an investigation made in the 4- by 4-foot supersonic pressure tunnel to determine the effects of body camber and body indentation on the longitudinal characteristics of a delta-wing-body combination at Mach number 1.61. Three bodies were tested with a 3-percent-thick 60 degree delta wing: a basic parabolic body, a body indented so as to have an improved wing-body area distribution at Mach number 1.8, and a body which was both indented and cambered. Results indicated that none of the changes had any appreciable effect at Mach number 1.61 on the minimum drag or maximum lift-drag ratios of the configurations tested." @default.
- W1783371072 created "2016-06-24" @default.
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- W1783371072 date "1956-04-20" @default.
- W1783371072 modified "2023-09-27" @default.
- W1783371072 title "Investigation of the effects of body camber and body indentation on the longitudinal characteristics of a 60 degree delta-wing-body combination at a Mach number of 1.61" @default.
- W1783371072 hasPublicationYear "1956" @default.
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