Q2: Answer One Section only. A: Determine (h) and gage pressure (A& B), if gage pressure at (A) increased by 45% from pressure B. (See Fig.2) B: Answer with True (T) or False (F). 1- Manometer and Piezometer used for determine large discharge at any point. 2- Gage pressure at any point larger than Absolute pressure. 3- Non-Uniform Steady State flow when = 0 and + 0. 4- Laminar flow when Viscosity Force larger than Initial Force. 5- Hydraulic Grade Line for ideal fluid=+Z+ 6- At Nozzle pressure-0. 7- Stagnation point mean pressure=0. 8- If D1 > D2 Q1< Q2. 9- Negative sign (-) for horizontal accelerationpressure is decrease. 10- Transition flow when 20000 < Re < 40000.
Q2: Answer One Section only. A: Determine (h) and gage pressure (A& B), if gage pressure at (A) increased by 45% from pressure B. (See Fig.2) B: Answer with True (T) or False (F). 1- Manometer and Piezometer used for determine large discharge at any point. 2- Gage pressure at any point larger than Absolute pressure. 3- Non-Uniform Steady State flow when = 0 and + 0. 4- Laminar flow when Viscosity Force larger than Initial Force. 5- Hydraulic Grade Line for ideal fluid=+Z+ 6- At Nozzle pressure-0. 7- Stagnation point mean pressure=0. 8- If D1 > D2 Q1< Q2. 9- Negative sign (-) for horizontal accelerationpressure is decrease. 10- Transition flow when 20000 < Re < 40000.
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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Transcribed Image Text:Q2: Answer One Section only.
A: Determine (h) and gage pressure (A&B), if gage pressure at (A) increased by 45% from pressure B.
(See Fig.2)
B: Answer with True (T) or False (F).
1- Manometer and Piezometer used for determine large discharge at any point.
2- Gage pressure at any point larger than Absolute pressure.
3- Non-Uniform Steady State flow when = 0 and + 0.
ds
4- Laminar flow when Viscosity Force larger than Initial Force.
5. Hydraulic Grade Line for ideal fluid = +Z +
6- At Nozzle pressure 0.
7- Stagnation point mean pressure-0.
8- If D1 > D2 → Q1< Q2.
9. Negative sign (-) for horizontal accelerationpressure is decrease.
10-Transition flow when 20000 < Re < 40000.
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