ROSE-HULMAN INSTITUTE OF
TECHNOLOGY
ES202: Thermal & Fluid Systems — Spring 2006–2007
All material, except laboratory dates, is subject to
change. Reading and HW assignments and exam dates will be finalized approximately
one week before they appear on the schedule.
Schedule and
material below the darkened row has not been finalized.
Reading and HW assignments are found in the Çengel and
Turner text. Items marked with an asterisk (*) are available by clicking on the
link.
Revised —0715 — 17
May 2007
Class |
Date |
Day |
Reading to be Completed |
Lesson Objectives |
Homework to be |
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1 |
3-5 |
M |
- - - |
Introduction relation of ES201 and ES202/ES204 thermodynamics, fluid mechanics, and
heat transfer Fluid
Fundamentals (1) Definition of a fluid Conservation of mass for a differential
open system (control volume): field variables – density,
velocity, pressure continuity equation for an
incompressible fluid |
Set
#1* (Due class 3) |
2 |
3-6 |
T |
1-1 to 1-4; 10-1 to 10-3 |
Fluid
Fundamentals (2) Flow visualization pathline, streakline, streamline,
and timelines Motion of a fluid element (fluid
kinematics): translation vs. rotation
(vorticity) expansion/compression (dilation)
vs. angular deformation Stream function and the velocity field |
Set
#2* (Due class 4) |
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W |
|
Week 1 — ES204 Lab |
|
3 |
3-8 |
R |
10-4 to 10-6; 1-5 to 1-9 |
Fluid
Fundamentals (3) Shear stress and viscosity Newtonian fluid Conservation of linear momentum for a
differential open system (control volume): Navier-Stokes equation for an
incompressible fluid common modeling assumptions |
Set
#3* (Due class 5) |
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4 |
3-12 |
M |
2-8 to 2-10 |
Hydrostatics (1) pressure
variation in a stationary fluid scales for
reporting pressure – absolute vs. gage pressure pressure
measurement: barometers, manometers, and gages |
Set #4 (Due class 6) 2-75, 2-79 |
5 |
3-13 |
T |
11-1 to 11-2 |
Hydrostatics (2) pressure
distribution on a submerged surface resultant
force on a submerged plane surface magnitude,
line of action, and point of application |
Set #5 (Due class 7) 2-78, 2-101, 11-14 |
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W |
Week 2 — ES202 Lab · Download and read Chapter 7 on Dimensional Analysis and Modeling from Essentials of Fluid Mechanics by Cimbala and Cengel BEFORE coming to lab. This is a free chapter distributed by McGraw-Hill as a supplement for the current text. Use the link at left to download the PDF file for the chapter. · Data for use during lab period ---- Liquid Column Breakup · Falling Sphere Data obtained by Fluids’R’Us testing (EXCEL Spreadsheet). |
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6 |
3-15 |
R |
11-3 to 11-4 |
Hydrostatics (3) buoyancy
force (Archimedes’ principle) |
Set #6* (Due class
8) |
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7 |
3-19 |
M |
12-2 |
Bernoulli
equation (1) origin, limitations, and physical
interpretation static, dynamic, and stagnation
pressure pressure variation along a streamline energy form vs. pressure form vs. head
form pressure variation across streamlines, especially parallel streamlines |
Set #7* (Due class 10) 12-27, 12-35 Think about Concept
Questions 12-11C to 12-24C |
8 |
3-20 |
T |
12-3 |
Bernoulli
equation (2) examples: Pitot-static tube, flow in a
nozzle or venturi, siphons |
Set #8 (Due class 11) 12-38/39, 12-45, 12-46 |
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W |
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Week 3 —
ES202 Lab — Optional Q&A for exam material (See instructor) |
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9 |
3-22 |
R |
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Exam I --- Classes 1-6 (Ground
rules) |
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10 |
3-26 |
M |
12-4 ES201 Energy notes |
Mechanical
Energy Balance (1) Conservation of energy (CoE) and the
Mechanical Energy Balance (MEB) One-inlet/one-outlet steady-state system |
Set #10 (Due class 12) 12-59, 12-67 |
11 |
3-27 |
T |
12-1 |
Mechanical
Energy Balance (2) Pump/Turbine Efficiency |
Set #11 (Due class 13) 12-83/85, 12-74 |
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W |
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Week 4 — ES204 Lab |
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12 |
3-29 |
R |
14-1 to 14-3 |
Internal
Flow (1) inlet region: developing flow and viscous
boundary layer entrance length Reynolds number and the flow regimes: laminar,
transition, and turbulent laminar flow in circular and
non-circular ducts |
Set #12 (Due class 14) 12-55/56 |
13 |
4-2 |
M |
14-4 and 14-5 |
Internal
Flow (2) turbulent flow in circular and
non-circular ducts predicting major and minor head losses pipe flow: major losses (friction losses
in straight pipes) |
Set #13 14-37, 14-38, 14-45 |
14 |
4-3 |
T |
14-6 |
Internal
Flow (3) pipe flow: minor losses (fittings,
inlets, outlets) |
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Week 5 — ES202
Lab |
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15 |
4-5 |
R |
----- |
Internal
Flow (4) applications |
Set #15 (Due class 17) 14-69, 14-87 |
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Spring
Break |
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16 |
4-16 |
M |
5-4 ES201 energy notes |
Steady-flow
devices (1): Characteristics of Turbines, pumps, compressors, fans,
blowers Nozzles, diffusers, throttling valves Heat exchangers |
Set #16 (Due class 18) 14-79, 5-66, and 5-85 For 5-66 and 5-85 assume air is ideal gas with
constant room-temperature specific heats (just like we did in ES201) AND add
a part (c) calculate the entropy generation rate. |
17 |
4-17 |
T |
3-1 to 3-4 |
Pure
substance properties (1) State postulate of a simple,
compressible substance |
Set #17 (Due class 20) 5-121 and 5-132 (where
necessary treat water as an incompressible substance and air as an ideal gas
with constant specific heats) |
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W |
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Week 6 — ES204 |
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18 |
4-19 |
R |
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Fluid mechanics Q & A |
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19 |
4-23 |
M |
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Exam II – Classes 7-15 |
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20 |
4-24 |
T |
3-5 |
Pure
substance properties (2) |
TBA ????? |
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4-25 |
W |
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Week 7 —
ES202 Lab — Property Lookup Lab |
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21 |
4-26 |
R |
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Pure
substance properties (3) Problem solving using real substance
property tables |
5-11, 5-21, 5-107 |
22 |
4-30 |
M |
3-6, 3-7, 3-9, 3-10; |
Pure
substance (4) compressibility factor Z and the
generalized Z-chart specific heats ideal gas model use of average specific heat values use of ideal gas tables |
5-43, 5-213, 7-67 |
23 |
5-1 |
T |
3-11, 7-8; |
incompressible substance Isentropic
processes (1) Representation on T-s diagrams |
7-75, 7-97, 7-102 |
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5-2 |
W |
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Week 8 —
ES202 Lab |
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5-3 |
R |
8-1, 8-2, 8-7 and Cycle material in ES201 Notes |
Thermodynamics Cycles (1) Power
Cycles (Heat Engines) Carnot
Cycle Model
for a gas turbine --- Brayton Cycle |
Answer 8-62E for an
ideal cycle (ηcomp = ηturb = 100%) (Due class 26) |
|
25 |
5-7 |
M |
8-9 to 8-11 |
Thermodynamic
Cycles (2) Model for a steam power plant ---
Rankine Cycle |
8-110, 8-132 (Due class 27) |
26 |
5-8 |
T |
8-14 to 8-18 |
Thermodynamic
Cycles (3) Refrigeration/Heat-Pump Cycles Reversed Carnot Cycle Model for a home air conditioner or
heat pump --- Mechanical vapor-compression cycle |
---- |
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W |
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Week 9 — ES204 Lab |
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27 |
5-10 |
R |
15.1 to 15.4, 15-6 |
External Flow
(1) Drag vs. Lift Drag force components: pressure drag vs.
shear (friction) drag Drag coefficient – determined
empirically Pressure drag difference between slender and
blunt bodies (streamlining) flow separation and its dependence
on Reynolds number |
15-27, 15-65,
15-68 (Due
class 29) |
28 |
5-14 |
M |
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Exam III – Classes 16 – 26 See Learning Objectives for Classes 16
– 22 and Classes 23
– 26 |
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29 |
5-15 |
T |
15-5 |
External flow
(2) Shear (friction) drag development of boundary layer along
a surface special case: parallel flow over
a flat plate skin friction coefficient: local
versus average. |
15-47E, 15-52 (Not collected) |
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W |
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Week 10 — ES204 Lab |
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30 |
5-17 |
R |
15-7 |
External flow
(3) Lift – Origin of lift Lift coefficient Stall as a direct consequence of flow separation |
15-88, 15-89 (Not collected) |
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5-23 |
W |
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Final Exam
6 pm — 10 pm (Ground rules) |
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