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An airplane has a rectangular-platform wing that has an elleiptical spanwise lift distribution. the airplane has a mass of 1200 kg, a wing area of 20 m^2, and a wingspan of 14 m, and it is flying at 60 m/s at 3000 m altitude in a standard atmosphere. if the form drag coefficient is .01, calculate the total drag on the wing and the power (p=FV) necessary to overcome the drag.
a stack was sampled for 8 minutes. the gas velocity at stack conditions through the sampler was 15.0 ms and the area
a strain-rate dependence test is conducted on samples of al 6061-t6. two identical bars are tested. the first bar is
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fully developed laminar flow occurs in a pipe line. the fluid in the pipeline has a dunamic viscosity of 0.08 nsm2 and
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a 120-in long annealed rod with a cross-section area of 0.86 in2 extruded from 5083 aluminum alloy has been axially
an engineer is designing a hydraulic lift with a capacity of 10 tons. the moving parts of this lift weigh 1000lbf. the
find the entropy in a throttling process per unit mass for ammonia. take the inlet state as specified as saturated
Estimate the energy that must have been supplied to cause the specimen to reach failure.
a 10 m3 tank contains nitrogen r0.2969 kjkg-k0.2969 kpa-m3kg-k at 30degc and 600 kpa. some nitrogen is allowed to
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