Answer:
A. cosmetologists will have a set income.
Explanation:
Hope it helps if not i am really sorry.
Answer:
A,B.C are correct.
Explanation:
The given question can be explained as following-:
The wings have a curvature on them called 'camber', which in essence is half of a venturi create a high pressure area on the bottom of the wing, and a low pressure area on top of the wing. To generate additional lift, the wing's camber (curvature) is increased by extending (in an arc) the leading edge, which is typically done by forcing the leading edge out on tracks, or hinging them out.
The additional camber gives them the additional lift needed for safe operation and control at slower aircraft speeds as when taking off or landing.
Allow the wing to operate at a higher angle of attack. A higher coefficient of lift is produced as a product of angle of attack and speed, so by deploying slats an aircraft can fly more slowly or take off and land in a shorter distance
Therefore, all A,B,C options are correct.
Answer:
248.756 mV
49.7265 µA
Explanation:
The Thevenin equivalent source at one terminal of the bridge is ...
voltage: (100 V)(1000/(1000 +1000) = 50 V
impedance: 1000 || 1000 = (1000)(1000)/(1000 +1000) = 500 Ω
The Thevenin equivalent source at the other terminal of the bridge is ...
voltage = (100 V)(1010/(1000 +1010) = 100(101/201) ≈ 50 50/201 V
impedance: 1000 || 1010 = (1000)(1010)/(1000 +1010) = 502 98/201 Ω
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The open-circuit voltage is the difference between these terminal voltages:
(50 50/201) -(50) = 50/201 V ≈ 0.248756 V . . . . open-circuit voltage
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The current that would flow is given by the open-circuit voltage divided by the sum of the source resistance and the load resistance:
(50/201 V)/(500 +502 98/201 +4000) = 1/20110 A ≈ 49.7265 µA