FLUID MECHANICS FUND. (LL)-W/ACCESS4th EditionCENGEL Publisher: MCG CUSTOMISBN: 9781266016042
FLUID MECHANICS FUND. (LL)-W/ACCESS
Solutions for FLUID MECHANICS FUND. (LL)-W/ACCESS
Problem 1CP:
Discuss how nondimensalizsionalization of the Navier-Stokes equation is helpful in obtaining...Problem 3CP:
Expalain the difference between an “exact” solution of the Navire-Stokes equation (as discussed in...Problem 8CP:
A box fan sits on the floor of a very large room (Fig. P10-8C). Label regions of the flow field that...Problem 12P:
In Example 9-18 we solved the Navier-Stekes equatien for steady, fully develeped, laminar flow in a...Problem 14P:
A flow field is simulated by a computational fluid dynamics code that uses the modified pressure in...Problem 15P:
In Chap. 9(Example 9-15), we generated an “exact” solution of the Navier-Stokes equation for fully...Problem 18P:
A person drops 3 aluminum balls of diameters 2 mm, 4 mm and 10 mm into a tank filled with glycerin...Problem 28P:
Consider again the slipper-pad bearing of Prob. 10-26. Perform an order-of-magnitude analysis on the...Problem 29P:
Consider again the slipper the slipper-pad bearing of Prob. 10-26. (a) List appropriate boundary...Problem 35P:
Discuss what happens when oil temperature increases significantly as the slipper-pad bearing of...Problem 51CP:
Consider the flow field produced by a hair dayer (Fig. P10-51C). Identify regions of this flow field...Problem 52CP:
In an irrotational region of flow, the velocity field can be calculated without need of the...Problem 59P:
Consider the following steady, two-dimensional, velocity field: V=(u,v)=(12ay2+b)i+(axy2+c)j . Is...Problem 61P:
Consider a steady, two-dimensional, incompressible, irrotational velocity field specified by its...Problem 66P:
In an irrotational region of flow, we wtite the velocitv vector as ttie sradient of the i-a]^r...Problem 69P:
Water at atmospheric pressure and temperature (=998.2kg/m2) , and =1.003103 at free stream velosity...Problem 70P:
The stream function for steady, incompressible, two-dimensional flow over a circular cylinder of...Problem 72CP:
We usually think of boundary layers as occurring along solid walls. However, there are other flow...Problem 83P:
On a hot day (T=30C) , a truck moves along the highway at 29.1m/s. The flat side of the treated as a...Problem 84EP:
A boat moves through water (T=40F) .18.0 mi/h. A flat portion of the boat hull is 3.3 ft long, and...Problem 85P:
Air flows parallel to a speed limit sign along the highway at speed V=8.5m/s . The temperature of...Problem 86EP:
Air flows through the test section of a small wind tunnel at speed V=7.5ft/s 60680F And the length...Problem 88P:
Consider the Blasius solution for a laminar flat plate boundary layer. The nondimensional slope at...Problem 90P:
A laminar flow wind tunnel has a test is 30cm in diameter and 80 cm length. The air is at 20C . At a...Problem 91P:
Repeat the calculation of Prob. 10-90, except for a test section of square rather than round cross...Problem 95P:
In order to avoid boundary laver interference, engineers design a "boundary layer scoop" to skim off...Problem 97P:
The stramwise velocity component of steady, incompressible, laminar, flat plate boundary layer...Problem 98P:
For the linear approximation of Prob. 10-97, use the definition of local skin friction cofficient...Problem 100P:
One dimension of a rectangular fiat place is twice the other. Air at uniform. speed flows parallel...Problem 104P:
Static pressure P is measured at two locations along the wall of a laminar boundary layer (Fig....Problem 106CP:
For each statement, choose whether the statement is true or false, and discuss your answer briefly....Problem 108P:
Calculate the nine components of the viscous stress tensor in cylindrical coordinates (see Chap. 9)...Problem 109P:
In this chapter, we discuss the line vortex (Fig. 10-109) as an example of an irrotational flow...Problem 110P:
Calculate the nine components of the viscous stress tensor in cylindrical coordinates (see Chap. 9)...Problem 113P:
The streamwise velocity component of a steady incompressible. laminar. flat plate boundary laver of...Problem 114P:
For the sine wave approximation of Prob. 10-112, use the definition of local skin friction...Problem 116P:
Suppose the vertical pipe of prob. 10-115 is now horizontal instead. In order to achoeve the same...Problem 117P:
Which choice is not a scaling parameter used to o nondimensionalize the equations of motion? (a)...Browse All Chapters of This Textbook
Chapter 1 - Introduction And Basic ConceptsChapter 2 - Properties Of FluidsChapter 3 - Pressure And Fluid StaticsChapter 4 - Fluid KinematicsChapter 5 - Bernoulli And Energy EquationsChapter 6 - Momentum Analysis Of Flow SystemsChapter 7 - Dimensional Analysis And ModelingChapter 8 - Internal FlowChapter 9 - Differential Analysis Of Fluid FlowChapter 10 - Approximate Solutions Of The Navier–stokes Equation
Sample Solutions for this Textbook
We offer sample solutions for FLUID MECHANICS FUND. (LL)-W/ACCESS homework problems. See examples below:
Chapter 1, Problem 1CPChapter 1, Problem 23PChapter 1, Problem 31PChapter 1, Problem 55PChapter 1, Problem 71PChapter 2, Problem 1CPChapter 2, Problem 19PChapter 2, Problem 39PChapter 2, Problem 49P
Given information: The pressure of the air is 95 kPa, the initial temperature is 20°C, the final...Chapter 2, Problem 77PChapter 2, Problem 85PChapter 2, Problem 87PGiven information: The diameter of glass tube is 0.018 in, the contact angle with the glass is 140°,...Chapter 2, Problem 118PChapter 2, Problem 123PChapter 2, Problem 127PChapter 2, Problem 128PGiven: The shear stress used for the Herschel-Bulkley constitute model is τ=τν+K( du dy)m, Yield...Chapter 2, Problem 132PChapter 3, Problem 1CPChapter 3, Problem 26PChapter 3, Problem 48PChapter 3, Problem 49PChapter 3, Problem 51PChapter 3, Problem 55PChapter 3, Problem 67PChapter 3, Problem 72PChapter 3, Problem 78PChapter 3, Problem 79EPChapter 3, Problem 80PChapter 3, Problem 81PChapter 3, Problem 85PChapter 3, Problem 86PChapter 3, Problem 87PChapter 3, Problem 90PChapter 3, Problem 135PThe radius of the semi-circular gate is 0.5 m, specific gravity of fluid in section 1 is 0.91,...Chapter 3, Problem 146PChapter 4, Problem 1CPChapter 4, Problem 23PGiven information: The flow is symmetric about x axis. Write the expression for the two-dimensional...Given information: The fluid particle is located on the centre line. Write the expression for the...Chapter 4, Problem 58PChapter 4, Problem 66PThe shear strain rate is half of the rate of decrease of the angle between two perpendicular lines...The vector field of flow is V⇀=k(x2−y2)i⇀−2kxyj⇀ and the radius of curvature of streamline is R=[1+...Chapter 4, Problem 98PChapter 4, Problem 101PWrite the expression for the two dimensional Poiseuille flow. u=12μdPdx(y2−hy). Here, the distance...Given information: The velocity component along the x direction is...Chapter 4, Problem 120PChapter 4, Problem 121PChapter 5, Problem 1CPChapter 5, Problem 53PChapter 5, Problem 55PChapter 5, Problem 57EPChapter 5, Problem 62PChapter 5, Problem 80PChapter 5, Problem 84PChapter 5, Problem 88PChapter 5, Problem 89PChapter 5, Problem 98PChapter 5, Problem 109PChapter 5, Problem 114PChapter 5, Problem 115PChapter 5, Problem 116PChapter 5, Problem 136PChapter 6, Problem 1CPChapter 6, Problem 23PGiven information: The volume flow rate of the water is 35 L/s, the discharge area for the smaller...Chapter 6, Problem 57PChapter 6, Problem 67PChapter 6, Problem 69PChapter 6, Problem 70PChapter 6, Problem 77PChapter 6, Problem 78PChapter 6, Problem 89PGiven information: The length of the slit is 1.2 m, width of the rectangular slit is 5 mm, water...Chapter 6, Problem 96PChapter 7, Problem 1CPGiven information: The shaft power is W˙, the angular velocity is ω, the fluid density is ρ, the...Chapter 7, Problem 53PChapter 7, Problem 62PChapter 7, Problem 67PThe angular velocity is ω, the fluid density is ρ, the acceleration due to gravity id g, the radius...Chapter 7, Problem 74PGiven information: force pressure gradient =dPdxFlow : steady+ incomprssible down stream distance...In M-L-T system, force = mass×accelerationF = m × a{F} = {mass × meter sec 2}{F} = {M × L t 2}{F} =...Given Information: Top plate speed, Vtop Bottom plate speed, Vbottom Steady flow, incompressible, 2...Chapter 7, Problem 112PChapter 7, Problem 113PChapter 7, Problem 118PGiven information: The following figure shows that two parallel flat plates. Figure-( 1) Assume, at...Chapter 8, Problem 1CPChapter 8, Problem 61PChapter 8, Problem 73PGiven information: The temperature of the water is 70 °F, density of the water is 62.3 lbm/ft3,...Given information: The air discharge rate is 1.2 ft3/s, diameter of the vent is 5 in, length of the...Given information: The temperature of oil is 20°C, the height of cylindrical reservoir is 20 cm, the...Given information: The temperature of the water is 110°C, density of the water is 950.6 kg/m3,...Chapter 8, Problem 94PChapter 8, Problem 96PGiven Information: The diameter of the pipe is 6 cm, the length of the pipe is 33 m, the inlet...Chapter 8, Problem 136PChapter 8, Problem 137PGiven information: The diameter of the cast iron pipe is 0.35 m and the length of the cast iron pipe...Given information: The diameter of tank 1 is 30 cm, diameter of tank 2 is 12 cm, diameter of orifice...Chapter 8, Problem 153PGiven information: The swimming pool diameter is 10 m, the swimming pool height is 2 m, the...Chapter 8, Problem 159PThe following figure represents the branched pipes. Figure-(1) Write the expression for the area of...Chapter 9, Problem 1CPChapter 9, Problem 16PGiven information: The incompressible flow filed for which the velocity u component is u=ax2−bxy,...Given information: The velocity component in θ direction is equal to 0. Write the expression for...Given information: The diameter at the entrance of the nozzle is 0.50 in, the diameter at exit of...Chapter 9, Problem 87PChapter 9, Problem 93PGiven information: The flow is steady, laminar, two-dimensional and incompressible. The flow is...Chapter 9, Problem 101PChapter 9, Problem 102PChapter 9, Problem 103PGiven information: The assumptions made are stated below: The flow is parallel, steady, and laminar....Chapter 9, Problem 123PChapter 10, Problem 1CPGiven information: Actual stokes law is FD=3πμDV+(9π/16)ρV2D2. Three aluminum balls of diameters 2...First, we need to use continuity equation for velocity component. From continuity equation, We have,...Chapter 10, Problem 29PGiven: h0=sleeper pad=11000h1=final height of sleeper=12000 lenght=1.0 Concept Used: Convergence of...Chapter 10, Problem 62PChapter 10, Problem 69PChapter 10, Problem 90PChapter 10, Problem 91PChapter 10, Problem 97PChapter 10, Problem 108PChapter 10, Problem 110PChapter 10, Problem 113PGiven information: The density of air is 0.8588 kg/m3, the temperature of air is −50°C the pressure...Chapter 11, Problem 1CPChapter 11, Problem 41EPChapter 11, Problem 43PChapter 11, Problem 48PChapter 11, Problem 68PChapter 11, Problem 88PChapter 11, Problem 96PChapter 11, Problem 101EPGiven information: Length=3 m Diameter=0.5 m Atmospheric pressure=87 kPa Temperature=20∘C=295 K...Given information: Mass of tractor=17,000 kg Frontal area=9.2 m2 Rolling resistance coefficient=0.05...Given information: Diameter=2 mm ρs=2600 kgm3ρf=1274 kgm3 Vexperimental=3.2 mms μ=1 kgm⋅s Concept...Given information: The diameter of the first aluminum ball is 2 mm, the diameter of the second...Given information: The diameter of the ball is 2 mm, the density of the ball is 2700 kg/m3, the...Chapter 12, Problem 1CPGiven: Air pressure, air temperature and Mach number are 14 psia, 40°F and 2 respectively. Flow...Given: The upstream the shock is given by, Pressure of air P1=58kPa Temperature of air T1=270K Mach...Given: The properties of air are: k = 1.4R = 0.287 kJ/kg·K,cp = 1.005 kJ/kg·K The properties of...Chapter 12, Problem 102PGiven: Temperature T1 = 480R Velocity V1=100 m/s Pressure P1=8 psia Mach number Ma1=2.0 Force...Chapter 12, Problem 126EPGiven: Ambient temperature at inlet T1= 500 K Stagnation Pressure P01=P1=220 psia Exit pressure P2 =...Given: The properties of air: R =0.280 kJ/kg.K cp=1.005 kJ/kg.K k=1.33 Inlet Temperature T1=510K...Given: Mach number k=1.2,1.4 and 1.6 range of 0≤Ma≤1. Calculation: Equation is given by m. R T 0...Chapter 13, Problem 1CPGiven Information: The water flow rate is 10 m3/s and the bottom slope is 0.0015 Write the...Given Information: The figure below represents the cross -section of three channels. Figure-(1) The...Given Information: The figure below shows the cross -section of the channel. Figure-(1) The bottom...Chapter 13, Problem 61PChapter 13, Problem 85PGiven information: Velocity of water flow is 10 m/s, the flow depth is 0.65 m, the bump height is 30...Given Information: The flow depth of upstream weir is 5 ft and the height of the gate opening is 1.1...Given information: The flow depth before the jump is 0.7 m, the flow depth after the jump is 5 m,...Given information: The channel angle is 0.5°. Write the expression for flow rate using manning's...Chapter 13, Problem 140PGiven information: Water is flowing through a sluice gate, the velocity of water before reaching the...Chapter 13, Problem 143PChapter 13, Problem 144PGiven information: The height of bump is 20 cm, initial velocity of flow is 1.25 m/s, the flow depth...Chapter 13, Problem 167PChapter 14, Problem 1CPChapter 14, Problem 35EPChapter 14, Problem 36EPChapter 14, Problem 41PChapter 14, Problem 47EPChapter 14, Problem 55EPChapter 14, Problem 56EPChapter 14, Problem 57EPChapter 14, Problem 61PChapter 14, Problem 62PGiven information: The number of rotations of centrifugal pump is 750 rpm. The inlet radius is 12 cm...Given information: The number of rotations of centrifugal pump is 750 rpm. The inlet radius is 12 cm...Given information: The diameter of the turbine A is 1.50 mand the number of rotation for the turbine...Chapter 14, Problem 123PChapter 15, Problem 1CP
More Editions of This Book
Corresponding editions of this textbook are also available below:
Fluid Mechanics Fundamentals And Applications
3rd Edition
ISBN: 9789339204655
Fluid Mechanics Fundamentals and Applications - With Access
3rd Edition
ISBN: 9780077707569
Fluid Mechanics Fundamentals And Applications
3rd Edition
ISBN: 9780073380322
Loose Leaf For Fluid Mechanics Fundamentals And Applications
3rd Edition
ISBN: 9780077595463
Fluid Mechanics Fundamentals And Applications
3rd Edition
ISBN: 9780077595418
FLUID MECH.:FUND....(LL)-W/CODE>CUSTOM<
3rd Edition
ISBN: 9781260115055
Connect 1 Semester Access Card For Fluid Mechanics Fundamentals And Applications
3rd Edition
ISBN: 9780077670245
FLUID MECHANICS:FUND.+APPL.(LL)>CUSTOM<
3rd Edition
ISBN: 9781260244342
FLUID MECHANICS FUNDAMENTALS+APPS
4th Edition
ISBN: 2810022150991
FLUID MECHANICS FUNDAMENTALS+APPS
4th Edition
ISBN: 9781259877766
Loose Leaf For Fluid Mechanics: Fundamentals And Applications
4th Edition
ISBN: 9781260152067
FLUID MECHANICS--ACCESS CARD
4th Edition
ISBN: 9781264623600
FLUID MECHANICS FUND.+APPL.
4th Edition
ISBN: 9781260602616
FLUID MECHANICS ACCESS
4th Edition
ISBN: 9781260792744
Package: Loose Leaf For Fluid Mechanics Fundamentals & Applications With 1 Semester Connect Access Card
4th Edition
ISBN: 9781260170160
FLUID MECHANICS LOOSE LEAF W/ CONNECT
4th Edition
ISBN: 9781260855463
Fluid Mechanics: Fundamentals and Applications
4th Edition
ISBN: 9781259696534
FLUID MECHANICS-W/ACCESS
18th Edition
ISBN: 9781307018431
EBK FLUID MECHANICS: FUNDAMENTALS AND A
4th Edition
ISBN: 8220103676205
FLUID MECHANICS LL W/ACCESS
4th Edition
ISBN: 9781260256505
Fluid Mechanics: Fundamentals and Applications
4th Edition
ISBN: 9781259877827
FLUID MECHANICS CONNECT ACCESS
4th Edition
ISBN: 9781264049509
FLUID MECHANICS LOOSELEAF W/CONNECT
4th Edition
ISBN: 9781264049837
Connect Access for Fluid Mechanics
4th Edition
ISBN: 9781259877759
FLUID MECHANICS (LL) W/CONNECT
4th Edition
ISBN: 9781264123728
Fluid Mechanics with Student Resources DVD
2nd Edition
ISBN: 9780077295462
Related Mechanical Engineering Textbooks with Solutions
Still sussing out bartleby
Check out a sample textbook solution.
