Show the expression for mechanical efficiency of the rocket as η = 2 u v ( u 2 + v 2 ) Explain the reason for the value of η = 1 when u = v .

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Answer 1

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Chapter 14.3, Problem 14.104P

To determine

Show the expression for mechanical efficiency of the rocket as η=2uv(u2+v2)

Explain the reason for the value of η=1 when u=v.

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Problem (17): water flowing in an open channel of a rectangular cross-section with width (b) transitions from a mild slope to a steep slope (i.e., from subcritical to supercritical flow) with normal water depths of (y₁) and (y2), respectively. Given the values of y₁ [m], y₂ [m], and b [m], calculate the discharge in the channel (Q) in [Lit/s]. Givens: y1 = 4.112 m y2 = 0.387 m b = 0.942 m Answers: ( 1 ) 1880.186 lit/s ( 2 ) 4042.945 lit/s ( 3 ) 2553.11 lit/s ( 4 ) 3130.448 lit/s

Problem (14): A pump is being used to lift water from an underground tank through a pipe of diameter (d) at discharge (Q). The total head loss until the pump entrance can be calculated as (h₁ = K[V²/2g]), h where (V) is the flow velocity in the pipe. The elevation difference between the pump and tank surface is (h). Given the values of h [cm], d [cm], and K [-], calculate the maximum discharge Q [Lit/s] beyond which cavitation would take place at the pump entrance. Assume Turbulent flow conditions. Givens: h = 120.31 cm d = 14.455 cm K = 8.976 Q Answers: (1) 94.917 lit/s (2) 49.048 lit/s ( 3 ) 80.722 lit/s 68.588 lit/s 4

Problem (13): A pump is being used to lift water from the bottom tank to the top tank in a galvanized iron pipe at a discharge (Q). The length and diameter of the pipe section from the bottom tank to the pump are (L₁) and (d₁), respectively. The length and diameter of the pipe section from the pump to the top tank are (L2) and (d2), respectively. Given the values of Q [L/s], L₁ [m], d₁ [m], L₂ [m], d₂ [m], calculate total head loss due to friction (i.e., major loss) in the pipe (hmajor-loss) in [cm]. Givens: L₁,d₁ Pump L₂,d2 오 0.533 lit/s L1 = 6920.729 m d1 = 1.065 m L2 = 70.946 m d2 0.072 m Answers: (1) 3.069 cm (2) 3.914 cm ( 3 ) 2.519 cm ( 4 ) 1.855 cm TABLE 8.1 Equivalent Roughness for New Pipes Pipe Riveted steel Concrete Wood stave Cast iron Galvanized iron Equivalent Roughness, & Feet Millimeters 0.003-0.03 0.9-9.0 0.001-0.01 0.3-3.0 0.0006-0.003 0.18-0.9 0.00085 0.26 0.0005 0.15 0.045 0.000005 0.0015 0.0 (smooth) 0.0 (smooth) Commercial steel or wrought iron 0.00015 Drawn…

Answer 2

Question

Chapter 14.3, Problem 14.104P

To determine

Show the expression for mechanical efficiency of the rocket as η=2uv(u2+v2)

Explain the reason for the value of η=1 when u=v.

Expert Solution & Answer

Want to see the full answer?

Check out a sample textbook solution

See solution

Answer 3

Question

Chapter 14.3, Problem 14.104P

To determine

Show the expression for mechanical efficiency of the rocket as η=2uv(u2+v2)

Explain the reason for the value of η=1 when u=v.

Expert Solution & Answer

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Check out a sample textbook solution

See solution

Answer 4

Question

Chapter 14.3, Problem 14.104P

To determine

Show the expression for mechanical efficiency of the rocket as η=2uv(u2+v2)

Explain the reason for the value of η=1 when u=v.

Expert Solution & Answer

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Check out a sample textbook solution

See solution

Answer 5

Chapter 14.3, Problem 14.104P

To determine

Show the expression for mechanical efficiency of the rocket as η=2uv(u2+v2)

Explain the reason for the value of η=1 when u=v.

Answer 6

Chapter 14.3, Problem 14.104P

To determine

Show the expression for mechanical efficiency of the rocket as η=2uv(u2+v2)

Explain the reason for the value of η=1 when u=v.

Answer 7

Chapter 14.3, Problem 14.104P

To determine

Show the expression for mechanical efficiency of the rocket as η=2uv(u2+v2)

Explain the reason for the value of η=1 when u=v.

Answer 8

Expert Solution & Answer

Answer 9

Expert Solution & Answer

Answer 10

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Answer 11

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Show the expression for mechanical efficiency of the rocket as η = 2 u v ( u 2 + v 2 ) Explain the reason for the value of η = 1 when u = v .

Solution Summary: The author explains the reason for the value of eta =1 when u=v as no power associated with the exhaust.

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Show the expression for mechanical efficiency of the rocket as η=2uv(u2+v2)

Explain the reason for the value of η=1 when u=v.

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Chapter 14 Solutions

Show the expression for mechanical efficiency of the rocket as η = 2 u v ( u 2 + v 2 ) Explain the reason for the value of η = 1 when u = v .

Solution Summary: The author explains the reason for the value of eta =1 when u=v as no power associated with the exhaust.

Concept explainers

Videos

Show the expression for mechanical efficiency of the rocket as η=2uv(u2+v2) Explain the reason for the value of η=1 when u=v.

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Chapter 14 Solutions

Show the expression for mechanical efficiency of the rocket as η=2uv(u2+v2)

Explain the reason for the value of η=1 when u=v.