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5.1 Introduction The properties of airfoils are the same as the properties of a wing with infinite span. However, all real airplanes have wings of finite span. In the present chapter, we will apply our knowledge of airfoil properties to the analysis for finite wings. As we have mentioned in the previous chapter, the analysis for the aerodynamics of wings is separated in two steps.now, we are going on the second-step in Prandtl's philosophy of wing theory
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Step One: Leading-in Activities: 1. Watch the short movies of Chaplin. 2. Discussion: (1) What do the famous people's lives look like in your eye? (2) Do you want to be famous one day? Why or why not? And (3) What do you usually do in your
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Reading I The Weather Step-l Lead-in Questions 1, What is the impression of Englishmen on you? Deep, simple but narrow and conservative
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Guessing a particular solution. Recall that a general linear recurrence has the form: f(n)=a1f(n-1)+a2f(n-2)+…+aaf(n-d)+g(n) As explained in lecture, one step in solving this recurrence is finding a particular solu- tion; i.e., a function f(n)that satisfies the recurrence, but may not be consistent with the boundary conditions. Here's a recipe to help you guess a particular solution:
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1. You need to deposit a high quality (low electrical resistivity) Al film at a very high rate(v> I micron/min) and achieve good step coveage using sputter deposition. Referring to information in the class notes and text, answer the following three questions. (Grade will depend more on how you justify your design, rather than on its
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MEMS LAB SESSION 2 Undercut Silicon Nitride using KOH Etching OVERVIEW OF LAB SESSION: This lab session utilizes potassium hydroxide(koh) wet etching to undercut and release the silicon nitride cantilevers and fixed-fixed beams. In Step
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CRYSTAL GROWTH step Crystal and questlons 1. Reactants In molten form 2. Transport to s/L Interface TAS Increases AH decreases
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To study Text B in detail(that is, to get to know the uses of some key words and phrases and to know the four-step method to study
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Mathematical basis of stability analysis =f(x,y) system of two coupled differential equations y=g(x,y) step 1 find nullclines and fixed point(s)
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