Engineering, 05.10.2019 11:30 nakeytrag
The wing of an aircraft is approximately rectangular with a wingspan of 17.5m and a chord of 3m. the aircraft is flying at sea level with a velocity of 200 m/s. if the flow is completely laminar and incompressible, calculate the boundary layer thickness at the trailing edge and the total skin friction drag.
Answers: 1
Engineering, 04.07.2019 18:10
Water at 70°f and streams enter the mixing chamber at the same mass flow rate, determine the temperature and the quality of the exiting stream. 0 psia is heated in a chamber by mixing it with saturated water vapor at 20 psia. if both streams enters the mixing chamber at the same mass flow rate, determine the temperature and the quality of the existing system.
Answers: 2
Engineering, 04.07.2019 18:10
Manometers are good examples of measuring instruments, nowadays they are not as common as before. a)-capacitive probe gauges b)-gravitational gauges deformation ) gauges d)-digital gauges
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Engineering, 04.07.2019 18:10
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Engineering, 04.07.2019 18:10
What are the two (02) benefits, which may result from a successful implementation of preventive maintenance (pm) program in an organization? (clo3)a)- lean manufacturing b)-overlapping responsibilities c)-the planner is not qualified d)-accurate contractor information e)-reduction in equipment redundancies f)-accurate stores information
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The wing of an aircraft is approximately rectangular with a wingspan of 17.5m and a chord of 3m. the...
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