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- W2100663178 abstract "A 1000-ft hypervelocity range was used to obtain the free-flight static and dynamic stability and drag data presented for a 10° semiangle cone. Measurements indicate that the damping-in-pitch derivatives for the cone increase appreciably with increasing Mach number between M = 8 and 16 at a Reynolds number (based on model length and freestream conditions) of about 0.4 X 10 6. Further, Cma for the cone decreases significantly as the noseradius to base-radius ratio of the cone is increased up to 0.1 for amplitudes greater than about 5°. Comparisons of the range stability data with wind-tunnel data (involving sting-supported models) obtained in different test facilities indicate that appreciable differences in Cma and (C,mq + Cma) exist in some cases." @default.
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- W2100663178 date "1970-02-01" @default.
- W2100663178 modified "2023-09-27" @default.
- W2100663178 title "Free-flight investigation of the aerodynamic characteristics of a cone at high Mach numbers" @default.
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- W2100663178 doi "https://doi.org/10.2514/3.5659" @default.
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