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Course: PS 280, Spring 2011School: University of Illinois,...
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1 Record: Superpower?: The Amazing Race between China's Hare and India's Tortoise. By: Moores, Alan. Booklist, 11/1/2010, Vol. 107 Issue 5, p14, 1p; Abstract: Reviews book the "Superpower?: The Amazing Race between China's Hare and India's Tortoise," by Raghav Bahl.; (AN 55472306) Database: Academic Search Premier
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Coursehero >> Illinois >> University of Illinois, Urbana Champaign >> PS 280Course Hero has millions of student submitted documents similar to the one
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1 Record: Superpower?: The Amazing Race between China's Hare and India's Tortoise. By: Moores, Alan. Booklist, 11/1/2010, Vol. 107 Issue 5, p14, 1p; Abstract: Reviews book the "Superpower?: The Amazing Race between China's Hare and India's Tortoise," by Raghav Bahl.; (AN 55472306) Database: Academic Search Premier
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Illinois Tech - ECE - 407
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ShintoShinto The way of the gods Here, gods refer to Japans spirits (kami) History No known person or group as its founder. Its mysterious origins date back to the ancient people of Japan and their stories of how they world came into being. The people of
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actually, there are 4 options for every disaster which occurs:1) God didn't know it was going to happen. 2) God knew it would happen, but couldn't do anything about it. 3) God knew it would happen, and let it happen. 4) God caused it to happenBut God is
Olive-Harvey College - CCC - THEO - 156
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; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ;* BEGIN LICENSE BLOCK * Version: MPL 1.1/GPL 2.0/LGPL 2.1 The contents of this file are subject to the Mozilla Public License Version 1.1 (the "License"); you may not use this file ex
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University of Illinois, Urbana Champaign - AE - 312
University of Illinois, Urbana Champaign - AE - 312
University of Illinois, Urbana Champaign - AE - 312
University of Illinois, Urbana Champaign - AE - 312
University of Illinois, Urbana Champaign - AE - 312
University of Illinois, Urbana Champaign - AE - 312
University of Illinois, Urbana Champaign - AE - 312
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AE 312: EXAM I FORMAT J. C. Dutton(1) (2) The first exam will be on Friday, March 4th from 1:00 1:50 pm. The format for the exam is closed book, closed notes; however, the following materials may be used during the exam: (a) Isentropic and normal shock t
University of Illinois, Urbana Champaign - AE - 312
University of Illinois, Urbana Champaign - AE - 312
University of Illinois, Urbana Champaign - AE - 312
AE 312 EXAMPLES 1.J. C. DuttonIn an experiment to determine drag, a circular cylinder of diameter d was immersed in a steady, two-dimensional, incompressible flow. Measurements of velocity and pressure were made at the boundaries of the control surface
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AE 312 Property Trends in Isentropic Flow J.C. Dutton 1 1 1 1 1 1DivergingSection A>0 +X M<1 M>1 Subsonic Supersonic Diffuser Nozzle ConvergingSection A<0 +X M<1 M>1 Subsonic Supersonic Nozzle Diffuser
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AE 312Isentropic Flow Functions J.C. DuttonA 1 2 1 2 2 1 1 M 2 A * M 1 P 1 2 1 1 M P0 2 1 2 1 1 M 0 2 T 1 2 1 M T0 2 1 11 2 2 1 1 PA * 12 P0 A 1 2 M 1 M 2 1
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AE 312Mass Flow Functions J.C. Dutton m RT M PA m RT P0 AM 1 2 1 M 1 2 12 m RT0PA m RT0 1 2 M M 1 2 P0 A 1 2 2 1 M M 1 2 1Fliegner's Formulae: m RT0P0 A * 1 2 1 0.6847 for 1.4 2 1For air ( = 1.4, R = 287 m2/s2-K = 1716 ft2/s2-R): m T
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AE 312Normal Shock Functions 2 M 2 1 VRU D 1 RU 1 1 V 1 1 M2 U VRD RU 1PD 2 2 1 P 1 1 M RU 1 PU 2 1 M 2 1 TD 2 RU 1 T 1 M RU 1 2 TU M2 RU 1 M2 RU M2 RD2 1 2 2 1 M RU 1 P0 RD P0 RU 1 2 1 1 1 2 M RU 2 1 M2 1 2 1 RU 1 1 M RU 2 2 1 1 M2 1 RU 1 1
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University of Illinois, Urbana Champaign - AE - 312
University of Illinois, Urbana Champaign - AE - 311
University of Illinois, Urbana Champaign - AE - 311
Ae311 1st exam Closed book and notes Answer all 3 questions Show all assumptions, equations, and working. Question 1Fall 2008Oct 1st 2008a) (5 pts) Consider the flow in a clamped, horizontal pipe shown in Fig 1. Draw a suitable control volume for this
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AE311 Midterm I Conservation of mass dV + V ndS = 0 t V SEquation Sheet +.V = 0 t()Conservation of momentum V dV + V V ndS = p ndS + f dV + F viscous t V S S V u u p u u +w = +v +u + f x + (Fx ')viscous z y x x t v p v v v + f y + (F y ')viscous +
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AE311 Exam 2 Equation Sheet Uniform Flow from left to right Source Flow Vortex flow Doublet Vrcos ln r 2 2 Vr Vcos 2 rV - VsinVrsin 2 ln r 2 K sin 2 r 2 r K cos 2 r 2 K sin 2 r 2K cos 2 r Uniform Flow from left to right Source Flow Vortex flow D
University of Illinois, Urbana Champaign - AE - 311
University of Illinois, Urbana Champaign - AE - 311
Problem 4)Problem 5)Grading Rubric 1.8) Identifying fundamental dimensions: K=4 Identifying Physical variables: N=7 N-K PI1, PI2, PI3 Identify PI1 as dimensionless and solving for CD (or M or gamma) Identify PI2 as dimensionless and solving for M (or CD
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University of Illinois, Urbana Champaign - AE - 311
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AE311 Fall 2008Problem Set 4Due: Oct 22nd 2008, before class1. (15pts) Consider the incompressible, irrotational, two-dimensional flow, where the stream function is = 2 xy a) What is the velocity at x = 1, y = 1? At x = 2, y =1/2? Are these points on t
University of Illinois, Urbana Champaign - AE - 311
University of Illinois, Urbana Champaign - AE - 311
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University of Illinois, Urbana Champaign - AE - 311
AE311 Fall 2008Problem Set 6Due: Nov. 26th 2008, before class1. (20 pts) Consider an airplane that weights 14,700 N and cruises in level flight at 300 km/h at an altitude of 3000 m. The wing has a surface area of 17.0 m2 and an aspect ratio of 6.2. Ass
University of Illinois, Urbana Champaign - AE - 311
University of Illinois, Urbana Champaign - AE - 311
AE311 Fall 2008Problem Set 7Due: December 10th 20081. Anderson, Problem 19.1. (see Anderson p847 for a summary of results for turbulent flow over a flat plate) 2. Anderson, Problem 19.2a) 3. Derive the expression for displacement thickness from the con
University of Illinois, Urbana Champaign - AE - 311
CHAPTER I 90.4471 m /scc 1 m ilhr1(a) C r= -=1.3231.328, E mNoting that drag exists on both the b nlton~nd top surfaces, we have a" Df 2 q m S Cr= 2(1/2)(1 .23)(63.04)~(9.75)(1.6)(5.04 x I 0 ) =Note that turbulent skin friction i 6 .28 t i~ncsarg
University of Illinois, Urbana Champaign - AE - 311
AE311 Fall 2008Problem Set 1Due: 8 Sept 20081. (15 pts) Anderson 4th edition: Problem 1.7 2. (15 pts) Anderson 4th edition: Problem 1.9 3. (15 pts) The velocity field given in Problem 2.4 is called vortex flow, which will be discussed in Chapter 3. For
University of Illinois, Urbana Champaign - AE - 311
University of Illinois, Urbana Champaign - AE - 311
AE 321 - Theoretical questionsLast update: September 29, 20081) Vector calculus: TRUE/FALSE a) The inner product of two vectors is a vector b) The gradient of a scalar eld is a vector c) The divergence of a vector eld is a vector d) The curl of a vector
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AE 321 - Equation Sheet Final ExamN 0 1 2 3 4 order zero (scalar) one (vector) two three four transformation lawA=A Ai = ij A j Aij = ik jl Akl Aijk = il jm Aijkl = im jnknAlmn kp lq AmnpqTensor operations:rr a b = aibi[r ar b]ij= aib j[rr a
University of Illinois, Urbana Champaign - AE - 311
AE 321 Homework #6 Due: Friday October 24, 2008 Chapter 4: Material Behavior1. (Old exam question) (a) Determine the slope of the x vs. x curve in the elastic range if an isotropic homogeneous material is tested under the following stress state:x=2y=
University of Illinois, Urbana Champaign - AE - 311
AE 321 Homework 6 Solution 1. (a) Given: x 2 y 3 zE x x y z E x x x x 3 2 E x x 5 x 6 5 E x x 1 6 6E x x 6 5 6E where the slope is . 6 5 (b) assumptions: linear, elastic, isotropic, homogeneous1 W ij ij 2 1 1 ij ij ij kk 2 E E 1 1 ij ij ii kk E 2
University of Illinois, Urbana Champaign - AE - 311
AE 321 Homework #7 Due: Wednesday November 5, 2008 Chapters 5, 6: Problem formulation, Extension, Bending1. Find all boundary conditions on all surfaces of the hollow circular cylinder (inner radius a, outer radius b) shown below in both (i) Cartesian co
University of Illinois, Urbana Champaign - AE - 311
AE 321 Homework #7 Solution 1. The figure below shows both the Cartesian coordinates x, y, z and the cylindrical coordinates r , , z used to define the boundary conditions of the hollow circular cylinder.(i) (a)Boundary conditions in Cartesian coordinat
University of Illinois, Urbana Champaign - AE - 311
AE 321 Homework #8 Due: Monday November 17, 2008 Chapter 7: FailureNOTE: All questions in this homework have previously appeared in exams.1. A linear, elastic, isotropic and homogeneous solid circular cylinder of length L and radius R (no restriction on
University of Illinois, Urbana Champaign - AE - 311
AE 321 Homework 8 solution Chapter 7: Failure and Fatigue 1a. We start with the following trial solution. P 0 0 0 P 0 0 0 0 Note that the entries in the upper left of the stress tensor, i.e. 11 , 22 , 12 21 , arise from the in-plane hydrostatic case, an
University of Illinois, Urbana Champaign - AE - 311
AE 321 Homework #9 Due: Not Graded. Do NOT hand in. Chapters 6, 7, 8: Torsion, Plane Problems and other problems1. (a) Show that the stress function for the torsion of a long cylinder of solid triangular cross section (shown below) subjected to a given t