Answered: 71. Find the inlet cross-sectional-area…

71. Find the inlet cross-sectional-area for an airplane engine (p, = 1.31 P2, P2 = 99.8 kPa, T2 = 232 °C, v, = 109 m-s1, v2 = 811 m-s", A2 = 0.7 m², Fth = 33 kN). A*.'."

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

See similar textbooks

Related questions

Q: The effect of Cavitations is due to:

A: Cavitation: It is the phenomenon of formation of vapour bubbles of a flowing fluids in a region when…

Q: Q2: Find the piezometric head at tank (C), if the discharge in pipe (1) = (65 L/sec). Use (-0.025)…

A: 2) Given: find the piezometric head at tank c Q1= Discahrge in pipe 1=65…

Q: If the pump efficiency is 75 percent, the power motor required to drive it is:

Q: (a.) A fluid at P1, V1, flows through a sudden 2:1 contraction, with Az/A1 = 1/2 (see figure below).…

A: given; A2/A1=12KL=0.25∆P=P2-P1

Q: In Fig. (3) determine Ap between points A and B. All fluids are at 20°C. (Ym= 9.79 kN/m', YBenene =…

A: Weight density of water,γw=9.79 kN/m3=9790 N/m3 Weight density of Benzene, γBenz=8640 N/m3 Weight…

Q: 27. Engine of an airplane (v, = 102.5 m-s", v2 = 792 m-s", Ftn = 31.8 kN, A, = 2.88 A2, pi = 1.26…

Q: Q2:an iceberg ( =9 kN/m') floats in ocean water (@ 10 kN/m') with 3000m' of the iceberg protruding…

Q: .force on part (BC) In Fig. shown, find the reaction m EL. = 10.7 207 kPa Air oil. rid=0188 EL=3m…

A: Given: The air pressure inside the tank, P1 = 207 kPa The elevation of water in tank, H = 10.7 m The…

Q: Consider the two flows below involving a pipe and nozzle where the inlet area is greater than the…

Q: 50. Find the volume of a tank (T = 42 C°, the rate change of density = 3.7 kg-m3-s“, p = 713 kPa),…

Q: Q4. IF 1 Pa =1 N/m, how many pascals when atmosp

Q: using generalized Vogel's equation. The fol- ata are given: r pressure, p = 5,500 psia oint…

A: Well A : pwf1>pb J* =q1p¯ -pwf1 =4005500-4000=0.2667 stb/day/psi qb=J*p¯…

Q: Section 2: Numerical Response Q3 : If the flow into a wind turbine is 10 m/s, and the flow far…

A: Given:The upstream velocity of flow, The downstream velocity of flow,

Q: a) Water moves through a constricted pipe in steady, ideal flow. At the lower point shown in the…

Q: SC- 0.92 Find: gas W> loN fresure, P;? O- 1cm Sm water 2m 1,5m

Q: Fluid, in P₁ = 2500 kPa P₂ = negligible Q₂ = 0.10 m³/s Pfluid=719 kg/m³ Hfluid=2.92 x 10-4. Epipe =…

A: Inlet PressureAnd outlet pressureDensity of the fluidDynamic viscosity of the fluidAnd elevation at…

Q: In Prob. it would be difficult to solve for Ω because of itappears in all three of the dimensionless…

Q: Q4) A reservoir-pipe system given in the figure below. The air pressure in the tank is 25 N/em?.…

Q: r location hav The anemom recorded durin са imeter

A: 1. Given, v = 5.5 m/s r = 1.8 m If = 0.21 CT = 0.89 Tf = 0.8 (a) Power = 0.5 A v3 If…

Q: B EL? Q3: Answer ONE Section only. a. Three reservoirs are connected, if pipe (1) and pipe (3)…

Q: Q1/ For fig shown if water flow rate is 60 lit/s , Find (h) Note that Density: Pwater = 1 kg/m Pair…

Q: Assume 4 kg/s of fluid are moving through an insulated pipe under these conditions: v1 = 6 m/s and…

A: Given Data m= 4 kg/s u1= 40 J/kg V1= 6 m/s

Q: Q2: The pipe flow in Fig. 2 is driven by pressurized air in the tank. What gage pressure pl is…

Q: 1. A bubble (assuming perfectly spherical) was released from a depth of 120m in the body of water by…

A: (a) Write the expression of absolute pressure when bubble is released. Pabs=Patm+ρgh1

Q: Determine the pressure difference between point c and point d, if A is water, B is mercury…

Q: Q2: A: For the tanks-system shown below, write the equations (only) of the flow in each tank. Assume…

A: Given: For tank 1: Incoming flow rate→Q1i=5 gal/min Outgoing flow rate→Q1o=2+3=5 gal/min…

Q: 71. Find the inlet cross-sectional-area for an airplane engine (p, = 1.31 p2, P2 = 99.8 kPa, T2 =…

A: Solution First, calculate the mass flow rate m=ρ2A2v2=ρ11.310.7×811=433 ρ1

Q: L11 Consider a concentric shaft fixed axially and rotated inside a (cylinder.rsh.Tey are the radius…

Q: A l-m-diameter, 2-m-long cylinder floats in an open tank containing a liquid having a specific…

Q: If the inlet diameter of the holding tank is 35cm and the outlet diameter is 30cm and the diameter…

Q: Choose the correct answer to the following (solution is required): If we have (6 m³) of oil weight…

A: Given data Volume = 6m3 The weight of oil = 47000(N) The specific weight of water = 9790(N) Find…

Q: Q) find the pressure differential between pipes B and A 4 in. Oil 3 in. YH20 = 62.4 IbF/ft YHg = 847…

Q: cylindrical syringe is filled with oil and the density is 0.855 g/cm3. (a)What is the pressure of…

A: density = ρ = 0.855g/cm3 = 855 kg/m3 dai (d1 ) = 4.50 cm = 0.045 m dia (d2 ) = 1.25 cm = 0.0125 m…

Q: and ex

A: INTRODUCTION: define notch weir venturimeter orifice and pitot tube.

Q: Figure P8.13 provides steady-state operating data for a solar power plant that operates on a Rankine…

Q: The highest building in Montreal is the '1 square building', with a height of 203m. The atmospheric…

A: Given data:-Pressure at the streets, P1=9.9×104Padensity of air, ρ=1.2kg/m3acceleration due to…

Q: Compute the pressure @ point n ( Pn ) as shown by the differential manometer in KPa if pressure @…

Q: Gas turbine engine (T2 = 214 °C, v2 = 764 m-s“, A2 = 0.63 m?, Fth = 32.8 kN, A, = 3 A2, p1 = 1.17…

A: Solution First Calculate the mass flow rate m=ρ2A2v2=ρ11.170.63×764=411.38ρ1

Q: Q2) For the configuration shown, find the height h? [Take: Sm=13.6, a=3+0.03 (cm), b=3-0.03 (cm),…

Concept explainers

Pressure Vessels

The term pressure vessel refers to a closed container that contains gas or liquid at a different pressure than environment pressure. The pressure vessels have a wide scale of applications in our day-to-day lives and other industrial places. Some common examples of pressure vessels are gas cylinders, autoclaves, compressor vessels, etc.

Question

71. Find the inlet cross-sectional-area for an
airplane engine (p, = 1.31 P2, P2 = 99.8 kPa, T2 =
232 °C, v, = 109 m-s1, v2 = 811 m-s1, A2 = 0.7 m?,
Ftn = 33 kN). A*.
%3D
%3D
==

Expert Solution

This question has been solved!

Explore an expertly crafted, step-by-step solution for a thorough understanding of key concepts.

SEE SOLUTION Check out a sample Q&A here

Step 1

Step 2

Step 3

Step 4

Step 5

Step by step

Solved in 5 steps

SEE SOLUTION Check out a sample Q&A here

Knowledge Booster

Learn more about

Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.

Similar questions

Figure shows a gage for very low pressures, inventedin 1874 by Herbert McLeod. ( a ) Can you deduce,from the fi gure, how it works? ( b ) If not, read about it andexplain it to the class.
1. A 100-mm diameter plunger (section 1) is being pushed at 60 mm/s into a tank filled with a fluid with a fluid of SG = 0.68. If the fluid is incompressible, how many pounds per second is being forced out at section 2, D2 = 20 mm? Answer: 0.707 lbf/s
Pro er hydrant nozzle in Fig. 1 has inlet and outlet diameters, D₁ = 8 cm and D₂ 1.0 cm. Water at 20°C flows through the nozzle at 0.001 m³/s and exits to the atmosphere. The atmospheric pressure is 101.3 KPa. Neglect the weight of the piping and nozzle. Compute: a) The exit fluid velocity, V2, ( b) The inlet pressure, Pl c) The horizontal force which must be resisted by the = flange bolts S d) The moment acting on the flange neglect the weight of the hydrant and water 10 m 8 cm Fig. 1: Water hydrant 1
For the below low-speed wind tunnel (Fig. 1), Settling chamber (reservoir) V₁ PI Nozzle V₂ P2. A2 Test section Diffuser Figure 2: Low-Speed Wind Tunnel P3 A3 A) Derive a mathematical expression to determine the flow velocity at the test section? B) At the sea level conditions, calculate the velocity at the test section when A1/A2=10 and the pressure difference is 4.9 kPa? C) What is a critical Reynolds number on an airfoil? D) If the airfoil has a critical Reynolds number of 550,000, how far aft of the airfoil's leading edge will transition occur?
PROBLEM S5.3 A thin spherical vessel 1 m in diameter and 12 mm thick is filled with water. More water is pumped in until the pressure reaches 4 MPla. How much extra water is required to reach this pressure? (E = 205 GPa; v = 0.25; K = 2 GPa) [Ans. 1.526 x10-3 m³] Pause Brea Lock Pg Up Num Lock Home Insert
Fluid 10
H5.
Please Answer Q2.
Marked out of 1.00 Flag question A fluid jet (S=1.4) of velocity V, =20 m/st %3D20m/s impinges normal to a flat plate which moves to the right at velocity V =15 m/s. Find the horizontal force required to keep the plate moving at constant velocity, the jet area is 3 cm. Noude
Solve it..
Please anybody answer this ASAP,i need the answer in 40 min Air flows isentropically through a channel To = 310 ° C. The two ends have identical areas, namely A = 25 cm², pressure p1 = 160 kPa and p2 = 65 kPa Determine a). Mass flow rate, b). Throat area and C). Ma2
Fluid A oil. abs + Tatm.) : 8. In the figure whown, PluidA is oil (s.9. = 0.80), Fluid B is upecial gage liguid (s.g.:s.g=2A), and x- 1.45 m., determine the clevation z of Fluid A if the prassure at pt. nis 22.06/25 klag and it is three - fourts of the pressure at pt.m. 3. %3D Fluide) sgl. Z :?