際際滷

際際滷Share a Scribd company logo

cengel-fluid mechanics

Mohsen Hassan vand
Mohsen Hassan vand

This document contains 73 comments on "Fluid Mechanics Fundamentals and Applications" by Yunus Cengel and Michael Boles. The comments note typos, provide suggestions to improve clarity or accuracy, and point out places where figures or explanations could be enhanced. Suggestions include rephrasing sentences for correctness, modifying figures, and adding mathematical definitions or explanations for concepts like the Leibnitz theorem before applying it. The goal of the comments is to refine the technical details and explanations provided in the textbook.

1 of 22
Downloaded 99 times
1 Comments on FLUID MECHANICS FUNDAMENTALS AND APPLICATIONS 2nd edition (SI Units) McGraw-Hill, 2010 Yunus. A. Cengel and Michael. A. Boles By: Mohsen Hassan vand Saturday, February 28, 2015
2 1. Pg. 2 ,L3-L4 while the branch that deals with bodies in motion is called dynamics. while the branch that deals with bodies in motion under the action of forces is called dynamics. 2. Pg. 3, FIGURE 13 3. Pg. 10, FIGURE 117 National Committee from Fluid Mechanics Films National Committee for Fluid Mechanics Films 4. Pg. 10, P2, L 4 no-slip condition no-slip condition 5. Pg. 12, P5, L 7 The eddies produce shock waves that move upstream. The wake produces waves that move upstream Please see figure 67 in Van Dykes book [An Album of Fluid Motion] 6. Pg. 13, P3, L 7
3 The velocity profile develops fully and remains unchanged after some distance from the inlet (about 10 pipe diameters in turbulent flow, and less in laminar pipe flow, The velocity profile develops fully and remains unchanged after some distance from the inlet (about 10 pipe diameters in turbulent flow, and more in laminar pipe flow, Please see the sentence under the relation (8-7) in page 343. [That is: The entry length is much shorter in turbulent flow, as expected, and its dependence on the Reynolds number is weaker.] 7. Pg. 17, under relation (1-1) to accelerate a mass of 32.174 lbm (1 slug) ...to accelerate a mass of 1 slug (32.174 lbm) 8. Pg. 18, P3, L5 Therefore, the gravitational acceleration g at a location depends on the local density of the earths crust,. Therefore, the gravitational acceleration g at a location depends on latitude, Note: The local density of the earths crust has a very minute or negligible effect on the gravitational acceleration g. 9. Pg. 21, FIGURE 139 It is suggested that the formulae to be separated by commas (,). 10.Pg. 27, EXAMPLE 15, P3 this system of two nonlinear equations this system of equations ( one linear and one nonlinear) 11.Pg. 28, L4 Reporting results in more significant digits implies
4 Reporting results in more significant digits falsely implies. 12.Pg. 31, P1, L2 Regarding this phrase if the batteries in the stopwatch were weak, its accuracy could be quite poor, it seems that until the batteries voltage drop below a certain threshold value, the stopwatch will be almost pretty accurate. Toward the end of batteries life, when the batteries voltage falls below that threshold voltage, stopwatch runs slow and loses its accuracy. 13.Pg. 32, P1, L3 An atomic blast A nuclear blast 14.Pg. 34, in Probs.1-39 and 1-40 converstion conversion 15.Pg. 35, in Prob.1-56 FD=function (C Drag, A front,.) FD=FD (C Drag ,A front,.) 16.Pg. 40, L4 after (2-4) Ru = 8.314 kJ/kmol Ru= 8.314 kJ/kmol 揃 K 17.Pg. 40, L5 from bottom, krypton and even heavier gases such as carbon dioxide carbon dioxide and even heavier gases such as krypton Note: krypton (83.8 g/mol) is heavier than carbon dioxide (44 g/mol). 18.Pg. 44, L1 after (2-11) 19.Pg. 46, FIGURE 213,(a) and (b) ( ) ( ) .P P V V T T T
5 Note: 1T C , and the dimension of ( ) .P V T T is the dimension of volume. 20.Pg. 48, P1,L4 a slight rise in local pressure a slight change in local pressure 21.Pg. 48, FIGURE 214 should be corrected. 22.Pg. 49, L13, 2 2 ( )dV dV Note: 2 2dV VdV 23.Pg. 53, P3, L1 (and Pg. 61,second column, L6) The viscosity of a fluid is a measure of its resistance to deformation. The viscosity of a fluid is a measure of its resistance to the rate of deformation. 24.Pg. 60, EXAMPLE 2-7, last sentence after the formula, Therefore, if a hole is drilled in the tube, air will leak into the tube rather than water leaking out. Therefore, if a hole is drilled in the tube, air will leak into the tube and some water leaks out, until the free surface (or meniscus) stands on the level where the hole is drilled. 25.Pg. 61,P2, last L generating highly destructive, extremely high-pressure waves. generating highly destructive, extremely high-pressure shockwaves. 26.Pg. 63 , item 3, Y. A. Cengel Y. A. Cengel
6 27.Pg. 76, FIGURE 35 28.Pg. 78, FIGURE 39 with distance from the free surface with vertical distance from the free surface 29.Pg. 79, FIGURE 312 W rghA W ghA 30.Pg. 84, FIGURE 320 31.Pg. 105, relation (3-49) & Pg. 109, relation (3-64) Pressure variation Pressure distribution 32.Pg. 108, FIGURE 357 The distance between limit lines [for showing ,maxsz ] should be shorter and shifted to the right place. 33.Pg.123, FIGURES P3-112 and P3-113
7 The same modification should also be applied to Figures P3-150, P3-151. 34.Pg. 124, FIGURE P3-118 1 1 7 7 He air He airr r 35.Pg. 126, Prob3-135 It seems that another factor for water overflow from the service tube is bubble formation (when the water is boiling). Bubbles reduce the water apparent density [two-phase density], and therefore lift the water to higher elevations, both inside the teapot and outside the teapot in the service tube). 36.Pg. 127, Prob3-139 The figures in the table should be rearranged. 37.Pg. 131( and in middle parts of page 159) Reynolds transport theorem (RTT) Reynolds Transport Theorem (RTT) 38.Pg. 135, relation(4-10) ( ) ( , , ) , ,x y z x y z 39.Pg. 136, EXAMPLE 42, P5, We now calculate the acceleration two ways We now calculate the acceleration in two ways 40.Pg. 137, FIGURE 412 , 2 2 , 3 3t dt t t t dt t t t dt t t Note: Mathematically, 2 3 0dt dt dt adt . 41.Pg. 139,L4
8 computational fluid dynamics (CFD) Computational Fluid Dynamics (CFD) 42.Pg. 139,FIGURE 416 ( , )dr dx dy dr dx dy 43.Pg. 141,last P, L1 particle image velocimetry (PIV) Particle Image Velocimetry (PIV) 44.Pg. 142,FIGURE 423 45.Pg. 155, FIGURE 445 Very important: The fluid particles shown in this figure are misleading! Because one may mistakenly think that these fluid particles are all the same, but in different locations and moments, and therefore if an individual spherical fluid particle is followed on its path, that particle keeps its spherical shape and rolls down with a rotational speed toward downstream . But we know that fluid particles deform during motion [The overall motion of a particle is a combination of its rotation and deformation (+translational)]. The vorticity is just a local and instantaneous property or concept, and therefore we cannot trace a fluid particle in space and time (different locations and moments) and then to expect that it really rotates with rotational speed . Please note that in boundary layers the is most often very high and a fluid particle cannot roll down with that high rotational speed. 46.Pg. 157, in (4-34) and in Pg 158,example 4-9, relation(2) 0 0 47.Pg. 162, P3 In this paragraph it is referred to the Leibnitz theorem without giving any previous explanation about it. It is suggested to introduce it in a separate paragraph in one-
9 and three-dimensional forms mathematically [because the Leibnitz theorem is actually the General Transport Theorem], and then derive the Reynolds Transport Theorem from it as a special form { when the volume under consideration is a material volume Vm within the surface Sm and sv v . Leibnitz theorem or General Transport Theorem: 1D: 3D: where sv = local and instantaneous velocity of the control surface S. 48.Pg. 172, Prob 4-40 The velocity field should be modified as: / 2u K r . In this form, K is the line vortex strength. Note: Please see the form of the relation given for line source in Prob 4-41. 49.Pg. 174, FIGURE P4-53, and 50.Pg. 174, FIGURE P4-56 and 51.Pg. 178, Prob 4-93,
10 2 2 2 2 2 2 2 2 2 2B t A t B t A t e Ae e AeB B 52.Pg. 179, Prob 4-104 zu u 53.Pg. 185, P2, L8 Regarding the following sentence: However, in nuclear reactions, the mass equivalence of the amount of energy interacted is a significant fraction of the total mass involved. It can easily be shown that even in nuclear reactions, the mass equivalence of the amount of energy interacted is a small fraction of the total mass involved. 54.Pg. 188, FIGURE 5-8 m per unit mass =m/m=1 m per unit mass = m/ m=1 55.Pg. 190, EXAMPLE 51 56.Pg. 192, L4 from bottom of the page, Note that pressure itself is not a form of energy Note that pressure itself is not a form of energy but a measure of potential energy stored per unit volume. 57.Pg. 194, EXAMPLE 517 1 1 1 1 2 20 0 atm atm atm atmV V p p p p p p p p 58.Pg. 206, EXAMPLE 55 and thus 1V 0 compared to jV and thus 1V is negligible compared to jV
11 Note: If, for example, 1V 5and 2V 100 then 1V is negligible compared to 2V ( we cannot deduce that 1V 0 , because 1V 5 !) Pg. 206, EXAMPLE 56 and thus 1V 0 compared to jV ( the tank is very large relative to the outlet) and thus 1V is negligible compared to jV ( the tank diameter is very large relative to the outlet diameter) 59.Pg. 207,end parts of EXAMPLE 56 From conversion of mass From conservation of mass 60.Pg. 219, FIGURE 5-56 61.Pg. 221, EXAMPLE 511 irreversibilities such as friction and swirling, and thus for reversible flow we have irreversibilities such as friction and eddies, and thus for reversible adiabatic flow we have and 62.Pg. 224 63.Pg. 227, left column, last P, is the dynamic pressure, is brought to a stop
12 is the dynamic pressure, is isentropically brought to a stop 64.Pg. 229, FIGURE P520 or 65. Pg. 262, FIGURE 632 and(Pg. 215, FIGURE 550 ) 66.Pg. 323, Prob. 7-29, 67.Pg. 344, L1 after relation(8-10) This phrase dr, dx 0 is mathematically wrong, because by definition dr, dx are themselves r , x 0, respectively. Therefore, it is suggested to replace the first line after relation (8-10) by following phrase:
13 Considering and 68.Pg. 347, FIGURE 815 69.Pg. 347, relation (8-30) 70.Page352, FIGURE 821 The turbulent stress profile in practice is nearly vertical in the core region [since the eddy motion is dominant in this region, and the effect of fluid viscosity is negligible] and horizontal near the wall [due to viscose effects there], something like this: 71.Page366, TABLE 84
14 72.Page371, FIGURE 842 73.Page384, last P Note that the pressure dropnot..total pressure drop. Note that the pressure dropnot..total pressure loss. It is suggested to make distinguish between the two terms pressure drop and pressure loss by following definition: pressure drop is caused by kinetic or potential energy conversion (kinetic or potential energy increase) and it is recoverable, but pressure loss is caused by viscosity and it is non-recoverable (or irreversible, and it is completely lost). 74.Page422, relation(9-6) Note: In Taylor series, is a finite difference (not an infinitesimal difference). 75.Page424, FIGURE 96 76.Page425,426, regarding the paragraph after (9-10),
15 From (9-10), 1 D Dt and .v have the same order of magnitudes. Therefore it is wrong to say: if changes in the density of the material element are negligibly small compared to the magnitudes of the velocity gradients in .v as the element moves around, 1 0 D Dt , and the flow is approximated as incompressible. According to the relation 1 . D v Dt (which is used as a criterion to see if a flow is compressible or not), whenever .v is zero or near zero[ or identically 1 D Dt is zero or near zero ], the flow can be considered incompressible. 77.Page 427, P1 after relation(9-15) It seems that this statement is wrong: If the flow is approximated as incompressible, density is not a function of time or space. Thus 0 t in Eq. 95 Because when a flow is approximated as incompressible, it means that its material derivative is zero, 1 0 D Dt , not 0 t . Very Important: 0 t i n steady state flows or in flows with homogeneous density ( 0), i.e, when cte . In incompressible flows 0 D Dt , or equivalently . 0V t . That is, .V t (not 0 t ). Therefore, in incompressible flows, density could be a function of time and space. 78.Page 438, FIGURE 926
16 79.Page 443,(9-39) or 80.Page 443,(9-41) 81.Page 443, FIGURE 933 gravity gravityF dF 82.Page 444,(9-42)
17 or 83.Page 445,(9-49) and in FIGURE 936, 84.Page 446, FIGURE 937
18 85.Page 446, L1 after (9-52) It seems that the following sentence is wrong! Hydrostatic pressure P in Eq. 952 is the same as the thermodynamic pressure Because hydrostatic pressure varies with depth, but thermodynamic pressure is a function of temperature and doesnt vary with depth, and . 86.Page 447, last paragraph, L3 Newtonian fluids, defined as fluids for which the shear stress is linearly proportional to the shear strain rate. Newtonian fluids, defined as fluids for which the stress tensor is linearly proportional to the strain rate tensor. Please note that in Newtonian fluids we have both linear and shear stresses (i.e., stress tensor, and the stress tensor is linearly proportional to the strain rate tensor). 87.Page 447, FIGURE 938, Shear strain rate strain rate , Shear stress Stress , and shear stress as a function of shear strain rate. Stress as a function of strain rate. 88.Page 447, last sentence of the page: A fluid that returns (either fully or partially) to its original shape after the applied stress is released is called viscoelastic. A fluid that returns (partially) to its original shape after the applied stress is released is called viscoelastic. 89.Page 462, FIGURE 961,
19 Please see comment 84(regarding page 446, FIGURE 937) 90.Page 471, FIGURE 975, Please see previous comment and: /2 (on right face) and /2(on left face) / 2(on top face) and / 2(on bottom face) and P=.... xr xr xr xr xr xr rx rx rx rx rx rx d d d d 91.Page 473, L1 after relation(9) the error function (Cengel, 2003) the error function 92.Page 476, Prob. 9-9, Note: 2 3 2 2 and 3 ...dx xdx dx x dx Also, dx= -0.1 x= -0.1 and f(x0+dx) f(x0+ x) 93.Page 493, Relation (10-1) is not printed. 94.Page 495,second item under relation (10-6) a)
20 b) * * * * * ( . ) and PV V in Eq. 106 are also order of magnitude unity * * * * * ( . ) and PV V in Eq. 106 are also of order of magnitude unity 95.Page 505, in relations (10-19), (10-20), the relation before (10-25), and relation (10-26) and FIGURE 1023 and FIGURE 1026 0 0 96.Page 511, in FIGURE 1033, is missed. 97.Page 514,L3 For example, if 1and 2 are , then . A and B are arbitrary constants. For example, if 1 and 2 are , then 1 2A A C is . A and B ,C are arbitrary constants. 98.Page 531, bottom of the page CFO CFD 99.Page 535, EXAMPLE 109, L2 and in FIGURE 1084 The line drawn isnt chord line (The chord line is the straight line connecting leading and trailing edges.). 100. Page 544, FIGURE 10102 101. Page 555, in FIGURE 10122(b)
21 102. Page 560, in FIGURE 10128 and in relation(10-89) top topm dm Since this is an infinitesimal or differential quantity. 103. Page 571, in Prob. 10-15C; I ,II, III, IV should be rearranged. 104. Page 779, FIGURE 1428 Increasing velocity Increasing viscosity 105. Page 822, L6 steam turbines typically have two stages (high pressure and low pressure) steam turbines typically have two sections (high pressure and low pressure) and each section has multiple stages. Note: Each stage is composed of one row of stator blades and one row of rotor blades.
This document was created with Win2PDF available at http://www.win2pdf.com. The unregistered version of Win2PDF is for evaluation or non-commercial use only. This page will not be added after purchasing Win2PDF.

More Related Content

cengel-fluid mechanics

  • 1. 1 Comments on FLUID MECHANICS FUNDAMENTALS AND APPLICATIONS 2nd edition (SI Units) McGraw-Hill, 2010 Yunus. A. Cengel and Michael. A. Boles By: Mohsen Hassan vand Saturday, February 28, 2015
  • 2. 2 1. Pg. 2 ,L3-L4 while the branch that deals with bodies in motion is called dynamics. while the branch that deals with bodies in motion under the action of forces is called dynamics. 2. Pg. 3, FIGURE 13 3. Pg. 10, FIGURE 117 National Committee from Fluid Mechanics Films National Committee for Fluid Mechanics Films 4. Pg. 10, P2, L 4 no-slip condition no-slip condition 5. Pg. 12, P5, L 7 The eddies produce shock waves that move upstream. The wake produces waves that move upstream Please see figure 67 in Van Dykes book [An Album of Fluid Motion] 6. Pg. 13, P3, L 7
  • 3. 3 The velocity profile develops fully and remains unchanged after some distance from the inlet (about 10 pipe diameters in turbulent flow, and less in laminar pipe flow, The velocity profile develops fully and remains unchanged after some distance from the inlet (about 10 pipe diameters in turbulent flow, and more in laminar pipe flow, Please see the sentence under the relation (8-7) in page 343. [That is: The entry length is much shorter in turbulent flow, as expected, and its dependence on the Reynolds number is weaker.] 7. Pg. 17, under relation (1-1) to accelerate a mass of 32.174 lbm (1 slug) ...to accelerate a mass of 1 slug (32.174 lbm) 8. Pg. 18, P3, L5 Therefore, the gravitational acceleration g at a location depends on the local density of the earths crust,. Therefore, the gravitational acceleration g at a location depends on latitude, Note: The local density of the earths crust has a very minute or negligible effect on the gravitational acceleration g. 9. Pg. 21, FIGURE 139 It is suggested that the formulae to be separated by commas (,). 10.Pg. 27, EXAMPLE 15, P3 this system of two nonlinear equations this system of equations ( one linear and one nonlinear) 11.Pg. 28, L4 Reporting results in more significant digits implies
  • 4. 4 Reporting results in more significant digits falsely implies. 12.Pg. 31, P1, L2 Regarding this phrase if the batteries in the stopwatch were weak, its accuracy could be quite poor, it seems that until the batteries voltage drop below a certain threshold value, the stopwatch will be almost pretty accurate. Toward the end of batteries life, when the batteries voltage falls below that threshold voltage, stopwatch runs slow and loses its accuracy. 13.Pg. 32, P1, L3 An atomic blast A nuclear blast 14.Pg. 34, in Probs.1-39 and 1-40 converstion conversion 15.Pg. 35, in Prob.1-56 FD=function (C Drag, A front,.) FD=FD (C Drag ,A front,.) 16.Pg. 40, L4 after (2-4) Ru = 8.314 kJ/kmol Ru= 8.314 kJ/kmol 揃 K 17.Pg. 40, L5 from bottom, krypton and even heavier gases such as carbon dioxide carbon dioxide and even heavier gases such as krypton Note: krypton (83.8 g/mol) is heavier than carbon dioxide (44 g/mol). 18.Pg. 44, L1 after (2-11) 19.Pg. 46, FIGURE 213,(a) and (b) ( ) ( ) .P P V V T T T
  • 5. 5 Note: 1T C , and the dimension of ( ) .P V T T is the dimension of volume. 20.Pg. 48, P1,L4 a slight rise in local pressure a slight change in local pressure 21.Pg. 48, FIGURE 214 should be corrected. 22.Pg. 49, L13, 2 2 ( )dV dV Note: 2 2dV VdV 23.Pg. 53, P3, L1 (and Pg. 61,second column, L6) The viscosity of a fluid is a measure of its resistance to deformation. The viscosity of a fluid is a measure of its resistance to the rate of deformation. 24.Pg. 60, EXAMPLE 2-7, last sentence after the formula, Therefore, if a hole is drilled in the tube, air will leak into the tube rather than water leaking out. Therefore, if a hole is drilled in the tube, air will leak into the tube and some water leaks out, until the free surface (or meniscus) stands on the level where the hole is drilled. 25.Pg. 61,P2, last L generating highly destructive, extremely high-pressure waves. generating highly destructive, extremely high-pressure shockwaves. 26.Pg. 63 , item 3, Y. A. Cengel Y. A. Cengel
  • 6. 6 27.Pg. 76, FIGURE 35 28.Pg. 78, FIGURE 39 with distance from the free surface with vertical distance from the free surface 29.Pg. 79, FIGURE 312 W rghA W ghA 30.Pg. 84, FIGURE 320 31.Pg. 105, relation (3-49) & Pg. 109, relation (3-64) Pressure variation Pressure distribution 32.Pg. 108, FIGURE 357 The distance between limit lines [for showing ,maxsz ] should be shorter and shifted to the right place. 33.Pg.123, FIGURES P3-112 and P3-113
  • 7. 7 The same modification should also be applied to Figures P3-150, P3-151. 34.Pg. 124, FIGURE P3-118 1 1 7 7 He air He airr r 35.Pg. 126, Prob3-135 It seems that another factor for water overflow from the service tube is bubble formation (when the water is boiling). Bubbles reduce the water apparent density [two-phase density], and therefore lift the water to higher elevations, both inside the teapot and outside the teapot in the service tube). 36.Pg. 127, Prob3-139 The figures in the table should be rearranged. 37.Pg. 131( and in middle parts of page 159) Reynolds transport theorem (RTT) Reynolds Transport Theorem (RTT) 38.Pg. 135, relation(4-10) ( ) ( , , ) , ,x y z x y z 39.Pg. 136, EXAMPLE 42, P5, We now calculate the acceleration two ways We now calculate the acceleration in two ways 40.Pg. 137, FIGURE 412 , 2 2 , 3 3t dt t t t dt t t t dt t t Note: Mathematically, 2 3 0dt dt dt adt . 41.Pg. 139,L4
  • 8. 8 computational fluid dynamics (CFD) Computational Fluid Dynamics (CFD) 42.Pg. 139,FIGURE 416 ( , )dr dx dy dr dx dy 43.Pg. 141,last P, L1 particle image velocimetry (PIV) Particle Image Velocimetry (PIV) 44.Pg. 142,FIGURE 423 45.Pg. 155, FIGURE 445 Very important: The fluid particles shown in this figure are misleading! Because one may mistakenly think that these fluid particles are all the same, but in different locations and moments, and therefore if an individual spherical fluid particle is followed on its path, that particle keeps its spherical shape and rolls down with a rotational speed toward downstream . But we know that fluid particles deform during motion [The overall motion of a particle is a combination of its rotation and deformation (+translational)]. The vorticity is just a local and instantaneous property or concept, and therefore we cannot trace a fluid particle in space and time (different locations and moments) and then to expect that it really rotates with rotational speed . Please note that in boundary layers the is most often very high and a fluid particle cannot roll down with that high rotational speed. 46.Pg. 157, in (4-34) and in Pg 158,example 4-9, relation(2) 0 0 47.Pg. 162, P3 In this paragraph it is referred to the Leibnitz theorem without giving any previous explanation about it. It is suggested to introduce it in a separate paragraph in one-
  • 9. 9 and three-dimensional forms mathematically [because the Leibnitz theorem is actually the General Transport Theorem], and then derive the Reynolds Transport Theorem from it as a special form { when the volume under consideration is a material volume Vm within the surface Sm and sv v . Leibnitz theorem or General Transport Theorem: 1D: 3D: where sv = local and instantaneous velocity of the control surface S. 48.Pg. 172, Prob 4-40 The velocity field should be modified as: / 2u K r . In this form, K is the line vortex strength. Note: Please see the form of the relation given for line source in Prob 4-41. 49.Pg. 174, FIGURE P4-53, and 50.Pg. 174, FIGURE P4-56 and 51.Pg. 178, Prob 4-93,
  • 10. 10 2 2 2 2 2 2 2 2 2 2B t A t B t A t e Ae e AeB B 52.Pg. 179, Prob 4-104 zu u 53.Pg. 185, P2, L8 Regarding the following sentence: However, in nuclear reactions, the mass equivalence of the amount of energy interacted is a significant fraction of the total mass involved. It can easily be shown that even in nuclear reactions, the mass equivalence of the amount of energy interacted is a small fraction of the total mass involved. 54.Pg. 188, FIGURE 5-8 m per unit mass =m/m=1 m per unit mass = m/ m=1 55.Pg. 190, EXAMPLE 51 56.Pg. 192, L4 from bottom of the page, Note that pressure itself is not a form of energy Note that pressure itself is not a form of energy but a measure of potential energy stored per unit volume. 57.Pg. 194, EXAMPLE 517 1 1 1 1 2 20 0 atm atm atm atmV V p p p p p p p p 58.Pg. 206, EXAMPLE 55 and thus 1V 0 compared to jV and thus 1V is negligible compared to jV
  • 11. 11 Note: If, for example, 1V 5and 2V 100 then 1V is negligible compared to 2V ( we cannot deduce that 1V 0 , because 1V 5 !) Pg. 206, EXAMPLE 56 and thus 1V 0 compared to jV ( the tank is very large relative to the outlet) and thus 1V is negligible compared to jV ( the tank diameter is very large relative to the outlet diameter) 59.Pg. 207,end parts of EXAMPLE 56 From conversion of mass From conservation of mass 60.Pg. 219, FIGURE 5-56 61.Pg. 221, EXAMPLE 511 irreversibilities such as friction and swirling, and thus for reversible flow we have irreversibilities such as friction and eddies, and thus for reversible adiabatic flow we have and 62.Pg. 224 63.Pg. 227, left column, last P, is the dynamic pressure, is brought to a stop
  • 12. 12 is the dynamic pressure, is isentropically brought to a stop 64.Pg. 229, FIGURE P520 or 65. Pg. 262, FIGURE 632 and(Pg. 215, FIGURE 550 ) 66.Pg. 323, Prob. 7-29, 67.Pg. 344, L1 after relation(8-10) This phrase dr, dx 0 is mathematically wrong, because by definition dr, dx are themselves r , x 0, respectively. Therefore, it is suggested to replace the first line after relation (8-10) by following phrase:
  • 13. 13 Considering and 68.Pg. 347, FIGURE 815 69.Pg. 347, relation (8-30) 70.Page352, FIGURE 821 The turbulent stress profile in practice is nearly vertical in the core region [since the eddy motion is dominant in this region, and the effect of fluid viscosity is negligible] and horizontal near the wall [due to viscose effects there], something like this: 71.Page366, TABLE 84
  • 14. 14 72.Page371, FIGURE 842 73.Page384, last P Note that the pressure dropnot..total pressure drop. Note that the pressure dropnot..total pressure loss. It is suggested to make distinguish between the two terms pressure drop and pressure loss by following definition: pressure drop is caused by kinetic or potential energy conversion (kinetic or potential energy increase) and it is recoverable, but pressure loss is caused by viscosity and it is non-recoverable (or irreversible, and it is completely lost). 74.Page422, relation(9-6) Note: In Taylor series, is a finite difference (not an infinitesimal difference). 75.Page424, FIGURE 96 76.Page425,426, regarding the paragraph after (9-10),
  • 15. 15 From (9-10), 1 D Dt and .v have the same order of magnitudes. Therefore it is wrong to say: if changes in the density of the material element are negligibly small compared to the magnitudes of the velocity gradients in .v as the element moves around, 1 0 D Dt , and the flow is approximated as incompressible. According to the relation 1 . D v Dt (which is used as a criterion to see if a flow is compressible or not), whenever .v is zero or near zero[ or identically 1 D Dt is zero or near zero ], the flow can be considered incompressible. 77.Page 427, P1 after relation(9-15) It seems that this statement is wrong: If the flow is approximated as incompressible, density is not a function of time or space. Thus 0 t in Eq. 95 Because when a flow is approximated as incompressible, it means that its material derivative is zero, 1 0 D Dt , not 0 t . Very Important: 0 t i n steady state flows or in flows with homogeneous density ( 0), i.e, when cte . In incompressible flows 0 D Dt , or equivalently . 0V t . That is, .V t (not 0 t ). Therefore, in incompressible flows, density could be a function of time and space. 78.Page 438, FIGURE 926
  • 16. 16 79.Page 443,(9-39) or 80.Page 443,(9-41) 81.Page 443, FIGURE 933 gravity gravityF dF 82.Page 444,(9-42)
  • 17. 17 or 83.Page 445,(9-49) and in FIGURE 936, 84.Page 446, FIGURE 937
  • 18. 18 85.Page 446, L1 after (9-52) It seems that the following sentence is wrong! Hydrostatic pressure P in Eq. 952 is the same as the thermodynamic pressure Because hydrostatic pressure varies with depth, but thermodynamic pressure is a function of temperature and doesnt vary with depth, and . 86.Page 447, last paragraph, L3 Newtonian fluids, defined as fluids for which the shear stress is linearly proportional to the shear strain rate. Newtonian fluids, defined as fluids for which the stress tensor is linearly proportional to the strain rate tensor. Please note that in Newtonian fluids we have both linear and shear stresses (i.e., stress tensor, and the stress tensor is linearly proportional to the strain rate tensor). 87.Page 447, FIGURE 938, Shear strain rate strain rate , Shear stress Stress , and shear stress as a function of shear strain rate. Stress as a function of strain rate. 88.Page 447, last sentence of the page: A fluid that returns (either fully or partially) to its original shape after the applied stress is released is called viscoelastic. A fluid that returns (partially) to its original shape after the applied stress is released is called viscoelastic. 89.Page 462, FIGURE 961,
  • 19. 19 Please see comment 84(regarding page 446, FIGURE 937) 90.Page 471, FIGURE 975, Please see previous comment and: /2 (on right face) and /2(on left face) / 2(on top face) and / 2(on bottom face) and P=.... xr xr xr xr xr xr rx rx rx rx rx rx d d d d 91.Page 473, L1 after relation(9) the error function (Cengel, 2003) the error function 92.Page 476, Prob. 9-9, Note: 2 3 2 2 and 3 ...dx xdx dx x dx Also, dx= -0.1 x= -0.1 and f(x0+dx) f(x0+ x) 93.Page 493, Relation (10-1) is not printed. 94.Page 495,second item under relation (10-6) a)
  • 20. 20 b) * * * * * ( . ) and PV V in Eq. 106 are also order of magnitude unity * * * * * ( . ) and PV V in Eq. 106 are also of order of magnitude unity 95.Page 505, in relations (10-19), (10-20), the relation before (10-25), and relation (10-26) and FIGURE 1023 and FIGURE 1026 0 0 96.Page 511, in FIGURE 1033, is missed. 97.Page 514,L3 For example, if 1and 2 are , then . A and B are arbitrary constants. For example, if 1 and 2 are , then 1 2A A C is . A and B ,C are arbitrary constants. 98.Page 531, bottom of the page CFO CFD 99.Page 535, EXAMPLE 109, L2 and in FIGURE 1084 The line drawn isnt chord line (The chord line is the straight line connecting leading and trailing edges.). 100. Page 544, FIGURE 10102 101. Page 555, in FIGURE 10122(b)
  • 21. 21 102. Page 560, in FIGURE 10128 and in relation(10-89) top topm dm Since this is an infinitesimal or differential quantity. 103. Page 571, in Prob. 10-15C; I ,II, III, IV should be rearranged. 104. Page 779, FIGURE 1428 Increasing velocity Increasing viscosity 105. Page 822, L6 steam turbines typically have two stages (high pressure and low pressure) steam turbines typically have two sections (high pressure and low pressure) and each section has multiple stages. Note: Each stage is composed of one row of stator blades and one row of rotor blades.
  • 22. This document was created with Win2PDF available at http://www.win2pdf.com. The unregistered version of Win2PDF is for evaluation or non-commercial use only. This page will not be added after purchasing Win2PDF.