An engineer wants a 4000kg helicopter to fly horizontally (neither gaining nor losing altitude) and increase speed at a rate of 2.6 m/s2 despite experiencing a 1000N drag. How many forces are acting on the helicopter?

Are all the forces on the helicopter balanced?

What is the magnitude of the net force on the helicopter?

What is the strength of the horizontal thrust component?

What is the strength of the thrust?

At what angle, theta, does the helicopter need to tilt?

Attached is a screenshot of the question.

answer: 819.89 miles across america

step-by-step explanation:

the final amount you will pay is $68.04.

the tip is determined by the pre-tax amount, so we calculate the tip based on the original bill, not after we've added sales tax.

to find the tip:

we can divide 54.00 by 100 to get 1% of 54. then we multiply that by 18.

54 / 100 = .54

.54 x 18 = 9.72

tip = 9.72$

to find the tax:

we can divide 54.00 by 100 to get 1% of 54. then we can multiply that by 8 to get 8%.

54 / 100 = .54

.54 x 8 = 4.32

tax= 4.32

now we can add the tip and tax to the bill to get our total.

54 + 9.72 + 4.32 = 68.04

total: $68.04

step-by-step explanation:

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step-by-step explanation: