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- W2369805584 abstract "For rockets with fins stable, we usually take low-rotation to vanish the thrust offset, eccentric mass and aerodynamic offset for improving shooting precision and denseness. But while lowly rotating, rockets should avoid the oscillating angular velocity of them, or say, rockets' nutation angular attenuates immediately after they are shooted. Slender rockets with fins will vibrate at random during flying, so when the angular velocity of them is designed, the natural frequency should be also avoided to prevent themselves from oscillating in step structurally. In the paper ANSYS is used to calculate the natural frequency of the rocket and vibrating response, from which the best scheme of the angular velocity of the slender rocket will be determinated." @default.
- W2369805584 created "2016-06-24" @default.
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- W2369805584 date "2004-01-01" @default.
- W2369805584 modified "2023-09-28" @default.
- W2369805584 title "Determination of Angular Velocity of the Slow-rotation of Slender Rockets with the Fins" @default.
- W2369805584 hasPublicationYear "2004" @default.
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