# Register now to access 7 million high quality study materials (What's Course Hero?) Course Hero is the premier provider of high quality online educational resources. With millions of study documents, online tutors, digital flashcards and free courseware, Course Hero is helping students learn more efficiently and effectively. Whether you're interested in exploring new subjects or mastering key topics for your next exam, Course Hero has the tools you need to achieve your goals.

3 Pages

### FluidsII_final-07

Course: WSE ME 530.328, Spring 2009
School: Johns Hopkins
Rating:

Word Count: 1219

#### Document Preview

- 530.328 Fluid Mechanics II, 2007 Final Exam Closed books, closed notes. Each problem has the same weight. Time: 35 minutes or less. Develop your answers on the available place. (33%) NAME: ...................... 1. A rough pipe is connected to a pressurized vessel (gauge pressure p) as shown. The viscous water flow exits to atmospheric pressure at speed V below the water level at height h. About the speed V,...

Register Now

#### Unformatted Document Excerpt

Coursehero >> Maryland >> Johns Hopkins >> WSE ME 530.328

Course Hero has millions of student submitted documents similar to the one
below including study guides, practice problems, reference materials, practice exams, textbook help and tutor support.

Course Hero has millions of student submitted documents similar to the one below including study guides, practice problems, reference materials, practice exams, textbook help and tutor support.
- 530.328 Fluid Mechanics II, 2007 Final Exam Closed books, closed notes. Each problem has the same weight. Time: 35 minutes or less. Develop your answers on the available place. (33%) NAME: ...................... 1. A rough pipe is connected to a pressurized vessel (gauge pressure p) as shown. The viscous water flow exits to atmospheric pressure at speed V below the water level at height h. About the speed V, which of these statements is TRUE? (a) The speed V is larger than (b) The speed V is smaller than (c) The speed V is equal to (d) Cannot say (e) The velocity is smaller than 2( p ! patm ) / " + 2 gh . 2( p ! patm ) / " + 2 gh . 2( p ! patm ) / " + 2 gh . ( p ! patm ) / h + 2 "h . p h V 2. A pipe divides into two as shown, each arm discharging to atmospheric pressure. The flow rate at the entrance is Q0. All pipe segments have the same length, diameter and roughness. Which of the following statements is FALSE? (a) Q1=Q2 (b) pM-p N < p N-patm (c) p N<pM (d) pM-p N > p N-patm (e) Q2 =Q0/2 Q1 patm Q0 M N Q2 patm 3. A Pelton wheel deflects a water jet at 180 degrees as shown. Evaluate the reaction torque Tz applied at the support S. V, A, y H z x V, A, S H/3 4. The Concorde used to fly at supersonic speeds. From the figure below showing the Mach cone, estimate the Mach cone angle assuming standard atmospheric conditions everywhere. V=650 m/s 5. Why is oil generally considered to be a better lubricant than water? (a) Because as a side-product of gasoline refining process it is cheaper. (b) Because it increases the shear stresses needed to slide surfaces along each other. (c) Because oil heats up less and thus dissociation and ionization effects are prevented. (d) Because oils higher viscosity causes a larger pressure build-up between surfaces (e) Because oils higher viscosity causes a smaller pressure build-up between surgaces 6. Consider real flow over a cylinder. Which one of these statements is FALSE? (a) Bernoulli equation may be applied far from the cylinder in the flow in the front portion. (b) The boundary layer near the front stagnation point is nearly of constant height (c) The minimum pressure point in the flow occurs at infinity. (d) The drag coefficient at high Reynolds number may depend on Reynolds number (e) If the flow were modeled using potential flow, the resulting drag force would be zero. xB 7. How would compute the expression xA ) % !y " cy( dx \$ ' # !u & using discrete approximations. c is a constant, and u is a function of (x,y): N #1 & ui , j +1 " ui , j "1 " c ui +1, j " ui " 2 , j ( !y, (a) ) % 2 \$ ' i = 1 2 !x ( )( ) ) where !x = ( x A " x B ) / N and !y = y / c (b) (c) (d) ) % 2 !y (u \$ N i =1 N #1 i , j +1 & " ui , j "1 " cy j ( !x, ' ) where !x = ( x A " x B ) / N and y j = j !y ) % !y (u \$ i =1 2 #1 i + 1, j + 1 & " ui "1, j "1 " vi , j ui +1, j " ui "1, j ( !x, ' ( ) where !x = ( x A " x B ) / N and !y = y / c " (( u N i =1 i + 1, j + 1 ! ui !1, j !1 ! cui , j #x 2 , ) ) where #x = ( x A ! x B ) / N 8. The thermodynamic process associated with propagation of sound is: (a) Isothermal (constant T) (b) Isobaric (constant pressure) (c) Constant density (d) Isentropic (constant s) (e) Constant enthalpy 9. If M1>1, in the diverging nozzle shown (isentropic flow), which of the following is correct? (a) V2<V1 and p2<p1 (b) V2<V1 and p2>p1 (c) V2>V1 and p2<p1 1 2 (d) V2>V1 and p2>p1 (e) There must be a normal shock between 1 and 2 10. Express the of acceleration the rocket in terms of the variables given on the sketch (show control-volume used): External air density air Drag coeff = Cd Rocket cross-sect area = AR Rocket instantaneous velocity = U Total Mass = M g Gas density j Nozzle area A Exit velocity of gases relative to rocket = Vj 11. What does the integral shown below stand for? !! 2 "" !(h + 12 V )(V idA) CS (a) Total torque applied to control surface (b) Rate of change of kinetic energy in control volume (c) Flux of potential energy across control surface (d) Flux of kinetic, internal energy and flow-work across control surface (e) Has no physical meaning 530.328 - Fluid Mechanics II, 2006 Final Exam Open books, open notes. Each problem has approximately same weight. (67%) Time: 2.4 hrs. NAME................................................................. 1. (30%) An American west windmill is an axial turbine. Suppose it is operating at a constant angular velocity, 60 rpm and that at these conditions the wind velocity (axial velocity) at the rotor is 5 m/s (use air density of =1.2 kg/m3). Assume the flow occurs through an annulus of fairly small radius difference, i.e. you may use the mean radius for your analysis. The mean radius is Rm = 0.7 m, and the frontal cross-flow area is Ac = 1.3 m2. Naturally the wind enters the windmill without swirl. The mean blade angle at the back-side (2) is 300. (a) Determine the torque and power output generated by the windmill. (b) Determine the inlet angle of the blade (1) so that the incoming flow is well aligned with the windmill at the design condition for 60 rpm and wind-speed of 5 m/s. (c) Assume that the shaft is connected to a water pump and assume that the transmission and pump have 100% efficiency. To pump water through a 1-inch rough pipe (e/D = 0.001) of length 200 meters, what flow-rate can I get for my farm? Dont be afraid to iterate 1-2 times Ac=1.3 m2 V1 (magnitude 5 m/s) Rm= 70 cm =60 rpm 1=? Rm 2=30 0 V2 D=2.54 cm m L=200 m 2. (18%) During the design of a wind-tunnel experiment, we wish to ascertain how close a support structure T (whose 2-D shape is well approximated by a Rankine half-body) can be brought to the measurement point A located upstream, without affecting the velocity there by more than 5% (i.e. the velocity at A should only be changed by 5% as compared to its value if T was not there at all). The unperturbed velocity is U=20 m/s and the thickness of the structure is h=15cm. Use 2-D potential flow. (a) Find the source strength and placement distance s. (b) Find the minimum distance d for 5% disturbance. (c) Under these conditions, find the percentage (compared to 0.5U2) by which the pressure at A is perturbed by the presence of T. air, =1.2 kg/m3 U=20 m/s A T d=? s=? h=15 cm 3. (19%) A smooth converging nozzle is attached to a large tank of compressed air (ideal gas). The pressure in the tank is 300,000 Pa, and density is 4.0 kg/m3. The flow that is established is isentropic within the nozzle. The back pressure is atmospheric pressure (100,000 Pa) away from the nozzle exit. Point 1 is right at the nozzle throat. (a) Find the Mach number at point 1. Is the flow there subsonic, sonic, or supersonic? (b) Find the temperature 0 in the tank, and T1 at the nozzle throat. (c) Find the density 1 of the air at the nozzle throat. (d) Find the speed of sound c1 in the air at point 1. (e) Find the air speed at the nozzle, V1. (f) The area of the nozzle is A1=2. x 10-4 m2. Evaluate the mass flow rate exiting the tank. M1 = ? 1= ? T1 = ? c1 = ? V1 = ? m=? Air tank at p0 = 3.0 105 Pa 0= 4.0 kg/m3 T0 = ?? pb = 1.0 105 Pa A1 = 2.0 x 10-4 m2
Find millions of documents on Course Hero - Study Guides, Lecture Notes, Reference Materials, Practice Exams and more. Course Hero has millions of course specific materials providing students with the best way to expand their education.

Below is a small sample set of documents:

Johns Hopkins - WSE - ME 530.328
530.328 - Fluid Mechanics II Spring 2009 Homework #6 Compressible Flow Due date: Tuesday May 5th before 3pm with Katy in ME office Latrobe 223 Review material in section 12 and 13.1, 13.2 and 13.5 Problems: 12.36 12.48 13.4 13.10 13.18 13.22
Johns Hopkins - WSE - ME 530.328
530.328 - Fluid Mechanics II Spring 2009 Homework #5 Potential Flow - Due date: Thursday April 91. A flow field is formed by combining a clockwise vortex, with strength , located at the origin, and a uniform flow in the negative x direction (right to lef
Johns Hopkins - WSE - ME 530.328
530.328 - Fluid Mechanics II Spring 2009 Homework #4 Potential Flow - Due date: Thursday April 21. Determine whether the Bernoulli equation can be applied between different radii for the vortex flow fields (a) (b) r.2. A plane source, of strength q, is
Johns Hopkins - WSE - ME 530.328
530.328 - Fluid Mechanics II Spring 2009 Homework #3 Angular Momentum - Due date: Thursday March 5th.1. A pump is used to pump water with flow rate 0.1 . The impeller inlet radius is 80 mm and blade width is 40 mm. The impeller outlet radius is 250 mm an
Johns Hopkins - WSE - ME 530.328
530.328 - Fluid Mechanics II Spring 2009 Homework #2 - flow in pipes Due date: Thursday February 12 at/before noon (zero tolerance late policy) in Latrobe 223 ME department office (Ms. Katy Sanderson)1. A pipe flow with water at standard conditions is ge
Loyola Maryland - CS - CS 631
Loyola Colleg e Computer Scien ce Dep t Spring 2006CS631: Computing Fundamentals II Homework - Abstract Data Types Due: Next class period, Feb. 8th Assignment: 1. Page 216, number 9 and 10. I dont need the answer to 10 to be compiled and run, but would a
Loyola Maryland - CS - CS 631
Loyola College Computer S cience D ept Spring 2006CS631: Computing Fundamentals II Homework - Java review and recursion Due: Next class period, Feb. 3rd Assignment: 1. Page 164, number 3 2. Page 164, number 4 3. Page 165, number 5 4. Page 165, number 11
Loyola Maryland - CS - CS 631
Computer S cience D ept. Loyola College Spring 2006CS631: Computer Science II Midterm Spring Solutions I. Short answer 1. Which statement makes the most sense? Circle the answer. CS631 is-a fun class CS631 has-a fun class. is-a makes the most sense since
Loyola Maryland - CS - CS 631
CS631 Homework 10a (bina ry trees) solut ions Page 590, #2a pre, in and postorder trav ersals of tr ee in f igure 11-44 Pre: MGDAHK LTRVU W In : ADHEKLMTRUVW Post: AHDLKGUV RW TM Page 590, #3 Giv en the tree in figure 11-45: a. Which node must have th e i
Loyola Maryland - CS - CS 631
CS631 Homework 9 solutions Page 513, #8 Tr ace inser tion sor t on the fo llow ing data. Und erlined values hav e just been moved ther e. Initial array: 20 80 40 25 60 40 Pass 1: 20 80 40 25 60 40 Pass 2: 20 40 80 25 60 40 Pass 3: 20 25 40 80 60 40 Pass 4
Loyola Maryland - CS - CS 631
CS631 Homework 4 solutions 1. Conver t Linked List class to use object rather than in teger . This is posted to th e class w eb p age under Lab and Examp le Code, Homework folder . The k ey was rep lacing int by Object in the Link edList and n ode classes
UPenn - MATH - Statistics
Homework 4, Stat 541: Due Friday, Oct 16, 2009, 12 noon Linear Algebra and Linear ModelsStudent Name: (replace this with your name) October 6, 2009Instructions: Edit this LaTex le with your solutions and generate a PDF le from it. E-mail the PDF to the
UPenn - MATH - Statistics
Homework 2, Stat 541: Linear Algebra, Due Fri, Sept 25, 2009, 12 NoonYour Name: (replace this with your name) October 5, 2009Instructions: Edit this LaTex le by inserting your solutions after each problem statement. Generate a PDF le from it and e-mail
UPenn - MATH - Statistics
Homework 2, Stat 541: Linear Algebra Due Fri, Sept 25, 2009, 12 NoonYour Name: (replace this with your name) September 22, 2009Instructions: Edit this LaTex le by inserting your solutions after each problem statement. Generate a PDF le from it and e-mai
University of Texas - PHY - Physics 30
The Conditions for EquilibriumExpect static equilibrium whenever acelerationFnet = 0 net = 0a = cfw_ax ; ay ; az and angular acceleration are zero,The first of these equations gives you up to threeconditions (for x, y , and z components); the lower
University of Texas - PHY - Physics 30
Kinetic Variables for RotationAngular position (in radians)Angular displacement == 2 - 1Angular velocity = /t(instantaneous a.v.: t 0)Angular acceleration = /t(instantaneous a.a.: t 0)c L.Frommhold. p.27/27Distance Travelled Along the ArcRotat
University of Texas - PHY - Physics 30
Definition of MomentumThe momentum of a particle is defined asp=mvMomentum is a vector Newton's 2nd law F = m v/t may be rewrittenp F = tprovided mass does not change with time.Actually, this is the correct form of the 2nd lawc L.Frommhold. p.18/1
University of Texas - PHY - Physics 30
Work (in Physics)In Physics Work is defined asW = FA d cos c L.Frommhold . p.21/21No Work, but (Lots of) Sweat ?A person standing at the busstop may get tired, but he is doing no Work,W = FA d cos because d = 0.Even if he were walkinghome, W = 0
University of Texas - PHY - Physics 30
Circular Uniform MotionDistinguish speed v(a scalar) from velocity v (a vector). velocity constant: linear motionUniform motion keepsUniform circular motionkeeps speed constant (circular motion)c L.Frommhold. p.20/14Centripetal AccelerationAccele
University of Texas - PHY - Physics 30
What is Force ?Accordig to Webster, FORCE means many things: strength or energy exerted or brought to bear cause of motion or change active power capacity to persuade or convince legal efficacy (. . . a law still in force. . . ) military strength, etc.
University of Texas - PHY - Physics 30
AnnouncementDue to an accident, Prof. Kleinman will be unable toInstructor: L. Frommhold, RLM 10.324; 471 5100 email: frommhold@physics.utexas.edu office hours: MWF 1111:50 a.m. at RLM 10.324teach this PHY302K course. I have been asked by the Chairman,
UT Arlington - PHYS - PHYS 3313
Chapter 1 Homework ProblemsSection 1. Special Relativity 1. If the speed of light were larger than it really is, would relativistic phenomena be more or less conspicuous than they are now? Why? Section 2. Time Dilation 2. How fast would an athlete have t
UT Arlington - PHYS - PHYS 3313
Chapter 1 Homework Solutions1. All else being equal, relativistic phenomena would be less conspicuous if the speed of light were larger. We would have to obtain an even larger speed than we do now for relativistic effects to manifest themselves.2.t = t
UT Arlington - PHYS - PHYS 3313
Chapter 2 Homework Problems1. If Planck's constant were larger than it is, would quantum phenomena be more or less conspicuous than they are now? 2. (a)A typical AM radio frequency is 1000kHz. What is the energy in eV of photons of this frequency? (b) Wh
UT Arlington - PHYS - PHYS 3313
Chapter 2 Homework Solutions1. Planck's constant gives a measure of the energy at which quantum effects are observed. If Planck's constant had a larger value, while all other physical quantities such as, speed of light, remained the same; quantum effects
UT Arlington - PHYS - PHYS 3313
Chapter 3 Homework Solutions1. (book #3)2. (book #4)3. a) 1 keV is small compared to proton rest energy of ~1 GeV so nonrelativistic is fine. ==h = ph = 2mKEhc 2mc 2 KE1.24 10-6 eV m 2(9.38 106 )(1000)= 9.110-12 mb) 1 GeV is not small compared
UT Arlington - PHYS - PHYS 3313
Chapter 3 Homework Problems1. (book #3)2. (book #4)3. a) Find the de Broglie wavelength of a 1.00 keV proton. Is a relativistic calculation needed? B) Find the de Broglie wavelength of a 1.00 GeV proton. Is a relativistic calculation needed? 4. (book #
UT Arlington - PHYS - PHYS 3313
Chapter 4 Homework1. book #5) 7. A (muon) is in the n=3 state of a muonic atom whose nucleus is a proton. Find the wavelength of the photon emitted when the muonic atom drops to its ground state. In what part of the spectrum is this wavelength? 2. book#
UT Arlington - PHYS - PHYS 3313
Chapter 4 Homework Solutions1. (book #5)2. (book #9)3.1= R(1 1 1 1 - 2 ) = 1.097 107 m -1 ( 2 - 2 ) 2 3 nf ni nf 11 1 = 1.097 107 ( - ) = 1.52 106 m -1 4 9 -7 = 6.58 10 m 1 1 1 n = 1: = 1.097 107 ( - ) = 9.75 106 m -1 1 9 -7 = 1.03 10 m n= 2:4.12
UT Arlington - PHYS - PHYS 3313
Chapter 5 Homework Problems
UT Arlington - PHYS - PHYS 3313
Solutions Chapter 51. Book #22. Book #33. Book #74. Book #9Solutions Chapter 55. Book #106. Book #14Solutions Chapter 57. Book #198. Book# 219. Book# 25Solutions Chapter 510. Book #2911. Book #30
UT Arlington - PHYS - PHYS 3313
Physics 3313 - Lecture 2Wednesday August 26, 2009 Dr. Andrew Brandt 1. Special Relativity 2. Galilean Transformations 3. Time Dilation and Length Contraction8/26/20093313 Andrew Brandt1CH. 1 Relativity (Motion) What do we mean by motion? Throw a bal
UT Arlington - PHYS - PHYS 3313
Physics 3313 - Lecture 3Monday August 31, 2009 Dr. Andrew Brandt HW1 Assigned due 09/09/09 Relativistic momentum and energy8/31/20093313 Andrew Brandt1Velocity Addition (Appendix) ~Worth reading 1.6 on connection of electricity and magnetism; electr
UT Arlington - PHYS - PHYS 3313
Physics 3313 - Lecture 4Wednesday September 2, 2009 Dr. Andrew Brandt 1. 2. 3. 4. 5. 6.9/2/2009Forgot to work Ex. 1.5 Finish Ch. 1 HW 1 still due 09/09/09 Quiz on Ch. 1 Particle Properties of Waves Photoelectric Effect3313 Andrew Brandt1Units Use W
UT Arlington - PHYS - PHYS 3313
Physics 3313 - Lecture 5Wednesday September 9, 2009 Dr. Andrew Brandt 1. HW1 Due HW2 Assigned (9/16) 2. Faculty Research Expo Weds 4pm Thurs 3:30 SH101 (extra credit) 3. What is Light? 4. X-Rays 5. Compton Effect 6. Pair Production 3313 Andrew Brandt9/9
UT Arlington - PHYS - PHYS 3313
Physics 3313 - Lecture 6Monday September 14, 2009 Dr. Andrew Brandt 1. 2. 3. 4. 5. 6. 7. Finish Ch.2 Pair Production etc. HW CH 2 due weds 9/16 Quiz (review 1, give 2) Wave Properties of Particles de Broglie Waves Matter Waves Wave Equation 3313 Andrew B
UT Arlington - PHYS - PHYS 3313
Physics 3313 - Lecture 7Wednesday September 16, 2009 Dr. Andrew Brandt 1. 2. 3. 4. HW2 due and HW3 assigned Phase Velocity Wave Equation Group Velocity9/16/20093313 Andrew Brandt1Phase Velocity How fast do dB waves travel? Might guess wave has same
UT Arlington - PHYS - PHYS 3313
Physics 3313 - Lecture 8Monday September 21, 2009 Dr. Andrew Brandt 1. 2. 3. 4. 5. 6.9/21/2009HW 3 due Weds 23rd Diffraction Particle in a Box Uncertainty Principal and Examples The Electron Rutherford Scattering3313 Andrew Brandt1Diffraction: Davis
UT Arlington - PHYS - PHYS 3313
Physics 3313 - Lecture 9Wednesday September 23, 2009 Dr. Andrew Brandt 1. 2. 3. 4. HW4 due Weds Sep. 30 Rutherford Experiment Bohr Atom Quantum Mechanics9/23/20093313 Andrew Brandt1Rutherford ScatteringN ( ) = sin 4K KE 22 The actual result was v
UT Arlington - PHYS - PHYS 3313
Physics 3313 - Lecture 10Monday September 28, 2009 Dr. Andrew Brandt 1. 2. 3. 4. 5.9/28/2009HW4 due Weds Sep. 30, test on Ch 1-5 Oct. 14 Schrodinger's Equation Wave Function Properties Operators and Expectation Values Eigenfunctions and Eigenvectors33
UT Arlington - PHYS - PHYS 3313
Physics 3313 - Lecture 11Wednesday September 30, 2009 Dr. Andrew Brandt 0. HW 4 due today HW5 due 10/7 Test ch 1-5 10/14 1. Eigenvalues 2. QM Particle in a box 3. Finite Potential Well9/30/20093313 Andrew Brandt1Eigenvalues Solutions for Schrodinger
UT Arlington - PHYS - PHYS 3313
Equations Test 1 PHYS 3313c = 3.0 10 8 m / s m electron = 0 . 511 MeV2-19c2= 9 . 11 10-27- 31kgm proton = 938 MeV c = 1.67 10kg mneutrone = 1.6 10 Coulomb h = 6.63 10 -34 J.s = 4.14 10 -15 eV .s R = 1.097 10 7 m -1 (Work function ) : Platinum
UT Arlington - PHYS - PHYS 5307
UT Arlington - PHYS - PHYS 5307
UT Arlington - PHYS - PHYS 5307
UT Arlington - PHYS - PHYS 5307
UT Arlington - PHYS - PHYS 5307
UT Arlington - PHYS - PHYS 5307
UT Arlington - PHYS - PHYS 5307
UT Arlington - PHYS - PHYS 5307
UT Arlington - PHYS - phys1441
PHYS 1441 Section 002 Lecture #1Monday, Jan. 14, 2008 Dr. Jaehoon Yu Who am I? How is this class organized? What is Physics? What do we want from this class? Brief history of physics Standards and units Dimensional AnalysisToday's homework is homework #
UT Arlington - PHYS - phys1441
PHYS 1441 Section 002 Lecture #2Wednesday, Jan. 16, 2008 Dr. Jaehoon Yu Brief history of physics Standards and units Uncertainties Significant FiguresWednesday, Jan. 16, 2008PHYS 1441-002, Spring 2008 Dr. Jaehoon Yu1Announcements Reading assignment
UT Arlington - PHYS - phys1441
PHYS 1441 Section 002 Lecture #3Wednesday, Jan. 23, 2008 Dr. Jaehoon Yu Dimensional Analysis Trigonometry reminder Coordinate system, vector and scalars One Dimensional Motion: Average Velocity;Acceleration; Motion under constant acceleration; Free Fall
UT Arlington - PHYS - phys1441
PHYS 1441 Section 002 Lecture #4Monday, Jan. 28, 2008 Dr. Jaehoon Yu Some Fundamentals One Dimensional Motion Displacement Speed and Velocity Acceleration Motion under constant accelerationHomework #2 is due 9pm, next Monday, Feb. 4!Monday, Jan. 28, 20
UT Arlington - PHYS - phys1441
PHYS 1441 Section 002 Lecture #5Wednesday, Jan. 30, 2008 Dr. Jaehoon Yu Acceleration Motion under constant acceleration One-dimensional Kinematic EquationMotion under constant accelerationWednesday, Jan. 30, 2008PHYS 1441-002, Spring 2008 Dr. Jaehoon
UT Arlington - PHYS - phys1441
PHYS 1441 Section 002 Lecture #6Monday, Feb. 4, 2008 Dr. Jaehoon Yu Examples for 1-Dim kinematic equations Free Fall Motion in Two Dimensions Maximum ranges and heightsToday's homework is homework #3, due 9pm, Monday, Feb. 11!Monday, Feb. 4, 2008PHYS
UT Arlington - PHYS - phys1441
PHYS 1441 Section 002 Lecture #7Wednesday, Feb. 6, 2008 Dr. Jaehoon Yu Motion in Two Dimension Motion under constant acceleration Vector recap Projectile Motion Maximum ranges and heightsWednesday, Feb. 6, 2008PHYS 1441-002, Spring 2008 Dr. Jaehoon Yu
UT Arlington - PHYS - phys1441
PHYS 1441 Section 002 Lecture #8Monday, Feb. 11, 2008 Dr. Jaehoon Yu Components and unit vectors Motion in Two Dimensions Projectile Motion Maximum ranges and heights Newton's Laws of Motion Force Newton's Law of Inertia &amp; MassPHYS 1441-002, Spring 2008
UT Arlington - PHYS - phys1441
PHYS 1441 Section 002 Lecture #9Wednesday, Feb. 13, 2008 Dr. Jaehoon Yu Motion in Two Dimensions Projectile Motion Maximum ranges and heights Newton's Laws of Motion Force Newton's first law: Inertia &amp; Mass Newton's second lawPHYS 1441-002, Spring 2008
UT Arlington - PHYS - phys1441
PHYS 1441 Section 002 Lecture #10Monday, Feb. 25, 2008 Dr. Jaehoon Yu Newton's Laws of Motion Force Newton's first law: Inertia &amp; Mass Newton's second law of motion Newton's third law of motionToday's homework is homework #5, due 9pm, Monday, Mar. 3!Mo