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- W2315208099 abstract "AIAA, Aerospace Sciences Meeting and Exhibit, 34th, Reno, NV, Jan. 15-18, 1996 A joint computational-experimental investigation was conducted to study the dynamic spin behavior of afterbody geometries which may be suitable for hypervelocity gun-launched kinetic energy projectiles. Numerical pretest simulations were performed with a parabolized Navier-Stokes code. A supersonic blowdown wind tunnel was used to collect the experimental data. Several afterbody configurations were tested, including thick and thin fin sets and straked and grooved flares. The results of the investigation showed exponential behavior of the spin history as was expected. Excellent agreement between the data and the computations for static roll moment coefficient was obtained in most cases. Good agreement was obtained for both the steady-state spin rate and the time constant. Analytical models used to estimate and correlate the data also showed good agreement in predicting the steady state spin rate but were less accurate in predicting either the static roll coefficient or the time constant. (Author)" @default.
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- W2315208099 date "1996-01-15" @default.
- W2315208099 modified "2023-09-23" @default.
- W2315208099 title "An investigation of the spin dynamics of afterbody configurations for hypervelocity projectiles" @default.
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- W2315208099 doi "https://doi.org/10.2514/6.1996-68" @default.
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