MDCAT Physics MCQS Rotational and Circular Motion Online Test 7
the-direction-of-angular-momentum-of-a-body-moving-along-a-circle-is-3-a_-_perpendicular-to-the-plane-of-the-circle,the-direction-of-angular-velocity-is-along-the-3-a_-_axis-of-rotation,the-direction-of-angular-velocity-is-determined-by-3-a_-_right-hand-rule,the-diver-spins-faster-when-moment-of-inertia-becomes-3-a_-_smaller,the-expression-for-centripetal-force-is-given-by-3-a_-_5-c-28-mr-5-comega-5-e-2-5-c-29,the-expression-for-the-orbital-velocity-of-satellite-is-3-a_-_3-cimg-src-3-d-22-2-fimages-2-fmcqs-2-f-11-th-2-fphy-2-f-11-th-phy-ch-05-044-02-png-22-3-e,the-expression-for-the-orbital-velocity-of-satellite-is-given-by-3-a_-_5-c-28-v-3-d-5-csqrt-7-b-0-crac-7-bgm-7-d-7-br-7-d-7-d-5-c-29,the-expression-for-the-time-period-of-low-flying-satellite-put-into-the-orbit-is-3-a_-_5-c-28-t-3-d-0-crac-7-b-2-5-cpi-r-7-d-7-bv-7-d-5-c-29,the-force-needed-to-kept-the-body-into-circular-motion-is-called-3-a_-_centripetal-force,the-formula-for-speed-of-satellite-orbiting-around-the-earth-is-3-a_-_5-c-28-v-3-d-5-csqrt-7-bg-r-7-d-5-c-29,the-frequency-of-rotation-of-a-spaceship-about-its-own-axis-to-create-artificial-gravity-like-that-on-earth-is-3-a_-_5-c-28-f-3-d-0-crac-7-b-1-7-d-7-b-2-5-cpi-7-d-5-csqrt-7-b-0-crac-7-bg-7-d-7-br-7-d-7-d-5-c-29,the-height-of-the-geostationary-satellite-above-the-equator-is-3-a_-_36000-km,the-largest-satellite-system-is-managed-by-3-a_-_126-countries,the-linear-velocity-of-a-disc-moving-down-an-incline-plane-is-3-a_-_5-c-28-5-csqrt-7-b-0-crac-7-b-4-7-d-7-b-3-7-dgh-7-d-5-c-29,the-magnitude-of-centripetal-force-on-a-mass-22-m-22-moving-with-angular-speed-22-5-c-28-5-comega-5-c-29-22-in-a-circle-of-radius-22-r-22-is-3-a_-_5-c-28-mr-5-comega-5-e-2-5-c-29,the-magnitude-of-centripetal-force-on-a-mass-27-m-27-moving-with-angular-speed-27-cf-89-27-in-a-circle-of-radius-27-r-27-is-3-a_-_3-cimg-src-3-d-22-2-fimages-2-fmcqs-2-f-11-th-2-fphy-2-f-11-th-phy-ch-05-023-02-png-22-3-e,the-mass-of-earth-is-equal-to-3-a_-_6-c-3-97-10-3-csup-3-e-24-3-c-2-fsup-3-e-kg,the-maximum-velocity-necessary-to-put-a-satellite-into-orbit-is-3-a_-_7-9-26-nbsp-3-bkms-3-csup-3-e-1-3-c-2-fsup-3-e,the-min-number-of-communication-satellites-required-to-cover-whole-earth-is-3-a_-_3,the-minimum-number-of-communication-satellites-required-to-cover-whole-earth-is-3-a_-_3,when-a-body-moves-in-a-circle-2-c-the-angle-between-linear-velocity-27-v-27-and-angular-velocity-27-cf-89-27-is-3-a_-_90-c-2-b-0,which-one-of-the-following-is-not-directed-along-the-axis-of-rotation-3-f_-_centripetal-acceleration
Questions | 22 |
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Available | Always |
Pass rate | 45 % |
Backwards navigation | Allowed |