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Rutgers - PSYCH - 300
Principles Principles of Corporate FinanceNinth EditionChapter 3How To Calculate Present ValuesSlides by Matthew WillMcGrawHill/IrwinCopyright2008byTheMcGrawHillCompanies,Inc.Allrightsreserved3- 2Topics Covered Valuing Long-Lived Assets Looking f
Rutgers - PSYCH - 300
Principles Principles of Corporate FinanceNinth EditionChapter 4Valuing BondsSlides by Matthew WillMcGrawHill/IrwinCopyright2008byTheMcGrawHillCompanies,Inc.Allrightsreserved4- 2Topics Covered Using The Present Value Formula to Value Bonds How Bo
Imperial College - AE - A.213
05/02/2009Before we startStructural Mechanics and DynamicsOverall Structural AnalysisLecture 1/5Course notes Tutorial sheetsgeneral office general office / intranet intranetWorked out solutions Lecture PPTs1Dr Silvestre Pinhointranet2Introduct
Imperial College - AE - A.213
05/03/2009Overview of last lectureStructural Mechanics and DynamicsStructural DynamicsLecture 2/7Dr Silvestre Pinho1 2Overview of last lectureOverview of last lecture34Overview of last lectureOverview of last lectureNumber of DOFs number of i
Imperial College - AE - A.213
05/03/2009Overview of last lecturesStructural Mechanics and DynamicsStructural DynamicsLecture 3/7Dr Silvestre Pinho1 2Overview of last lecturesOverview of last lectures& r In general: M & + C r + K r = R()Potential energy StiffnessKinetic ener
Imperial College - AE - A.213
05/03/2009Overview of last lecturesStructural Mechanics and DynamicsStructural DynamicsLecture 4/7& r In general: M & + C r + K r = R()M, C and K are always symmetric Mass assumed lumped at points M diagonalDr Silvestre Pinho1 2Overview of last l
Imperial College - AE - A.213
05/03/2009Overview of last lectures0000000000000000000 0000000000000000000000000000000000000 0000000000000000000 0000000000000000000 0000000000000000000000000000000000000 0000000000000000000 0000000000000000000 0000000000000000000000000000000000000 0000
Imperial College - AE - A.213
05/03/2009Overview of last lecturesStructural Mechanics and DynamicsStructural DynamicsLecture 6/7Free vibrationsDiscrete systems (n DOFs)Periodic loadingTransient loadingDr Silvestre Pinho1 2Overview of last lecturesDiscrete systems (n DOFs)
Imperial College - AE - A.213
05/03/2009Overview of last lecturesStructural Mechanics and DynamicsStructural DynamicsLecture 7/7Free vibrationsDiscrete systems (n DOFs)Continuous systemsPeriodic loadingTransient loadingFree vibrationsDr Silvestre Pinho1 2Objectives of thi
Imperial College - AE - A.213
08/02/2009Before we startStructural Mechanics and DynamicsOverall Structural AnalysisLecture 2/5Computational exercise: Instructions intranet intranetskeleton program & other filesDr Silvestre Pinho1 2Overview of last lectureOverview of last lec
Imperial College - AE - A.213
18/10/2009Structural Mechanics and DynamicsOverall Structural AnalysisLecture 3/5Dr Silvestre Pinho1Overview of last lecturesThe set of forces, R, and displacements, r, can be related in the stiffness formR = KrOr the flexibility formr = FRThe
Imperial College - AE - A.213
08/02/2009Overview of last lecturesStructural Mechanics and DynamicsOverall Structural AnalysisLecture 3/5The set of forces, R, and displacements, r, can be related in the stiffness formR = KrOr the flexibility formr = FRThe stiffness matrix of t
Imperial College - AE - A.213
08/02/2009Overview of last lecturesStructural Mechanics and DynamicsOverall Structural AnalysisLecture 4/5The set of forces, R, and displacements, r, can be related in the stiffness formR = KrOr the flexibility formr = FRDr Silvestre Pinho1 2Ov
Imperial College - AE - A.213
08/02/2009Overview of last lecturesStructural Mechanics and DynamicsOverall Structural AnalysisLecture 5/5Statically determinate systemR 100000000000 000000000000000000000 00 00 00 00 00 00 00 00 00 00 00 00000000000 000000000000000000000 000000000
Imperial College - AE - A.213
Mohrs Circle: DerivationThe stress transformation for 2D system is z 'z ' = zz cos 2 + ss sin 2 + zs sin 2 z 's ' =z's' zz zs o ds zs ss z'z'( zz+ ss ) sin 2 + zs cos 2 2dl dzThe first equation can be re-written as z 'z ' = zz (1 + cos 2 ) ss (1 c
Imperial College - AE - A.213
Imperial College - AE - A.213
Buckling AnalysisWhen a structure ( subjected to compression or shear ) undergoes visibly large displacements transverse to the load then it is said to buckle. Buckling may be demonstrated by pressing the opposite edges of a flat sheet of cardboard towar
Imperial College - AE - A.213
Imperial College - AE - A.213
Twisting of Single Cell Closed TubesThe unit load method then gives the section twist, , as1 = zs zs dVThe increase of twist, d , over a length dz of the tube is then zs =1 2 AtV zs =q (s ) GtdVSd =0S1 q (s ) tds dz = 2 At Gt0q (s ) ds dz
Imperial College - AE - A.213
Imperial College - AE - A.213
Imperial College - AE - A.213
Structural Mechanics and Dynamics AE213Professor Ferri M H Aliabadi1Course LayoutMain Topics covered are: Shear flow analysis for thin walled sections Structural failure assessment Buckling analysis2Shear flow analysis for thin walled sectionsThis
Imperial College - AE - A.213
Structural Mechanics and Dynamics 2nd Year Course NotesProfessor M H Aliabadi20091ContentsCONTENTS1Introduction.51.1 1.2 1.3 1.4 1.5 Influence of the Aircraft Shape on Aircraft Structural Analysis .6 Components of a Stressed Skin Structure.8 Loadi
Imperial College - AE - A.213
Example The Shear Flow in an Open Channel Section Subject to a Horizontal Shear Force Sxt 3 4The initial steps, 1 and 2, are identical to those of sectiontSy = 0 I xy = 0q( s) =Sx Dy I yyhSxt 2 d 1Step 3 Calculation of the D y DistributionD y (
Imperial College - AE - A.213
Smeared Stiffener IdealisationIf there are many closely spaced stiffeners then it can be assumed that their effect is distributed over the skin between the corner points. In this case, the effect of the stiffeners can be smeared over the skin and the eff
Imperial College - AE - A.213
Imperial College - AE - A.213
Structural Mechanics and Dynamics2nd Year Lecture Notes onOverall Structural AnalysisandStructural DynamicsDr Silvestre T Pinho(These notes are based on previous notes by D Hitchings)Thursday, 01 October 2009ContentsCONTENTS1 Overall Structural
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 1SolutionsQ1. Part 1 The unit virtual load R in a pin-jointed structure gives rise to a virtual load N i in memb
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 1Section a Theory Development 1. The principle of virtual work can be applied in two forms: a) Where the strains
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 1 1. Find, from first principles, the second moments of area of the sections shown in figures 1a and 1b. Both sect
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 2SolutionsQuestion 1 The real strains for a typical member is= N My + A IThe virtual stresses for the same mem
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 2 Section a Theory Development 1. The principle of virtual forces, in the form of the unit load method, gives the
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 2Section a Theory Development 1. Given that the shear flow is assumed to be zero at all but one free edge of an o
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 3SolutionsQ1. Convolution integralr (t ) = sin ( t ) R () d m 0twhere 2 = k m . In this case the force is con
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics Tutorial Sheet 3Section a Theory Development 1. It is common practice to estimate the effect of a suddenly applied loading on a str
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 3 6. Figure 1 shows the cross-section of a cantilever beam carrying a vertical shear load of 500N. Find the result
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 4 1. Find, from first principles, the second moments of area of the sections shown in figures 1a and 1b. Both sect
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 4 1. Idealise the tube cross-section of figure 1 of tutorial sheet 2 so that all of the direct stress carrying cap
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 5Section a Theory Development 1. Given that the shear flow is assumed to be zero at all but one free edge of an o
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 51. Determine the magnitude and direction of the maximum direct and shear stresses for each of the following two-
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 6 6. Figure 1 shows the cross-section of a cantilever beam carrying a vertical shear load of 500N. Find the result
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 61. Two rigid rods of equal length L are connected together with a pin and a rotational spring of stiffness k. Th
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 7 1. Idealise the tube cross-section of figure 1 of tutorial sheet 2 so that all of the direct stress carrying cap
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 81. Determine the magnitude and direction of the maximum direct and shear stresses for each of the following two-
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 91. Two rigid rods of equal length L are connected together with a pin and a rotational spring of stiffness k. Th
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 1SolutionsQuestion 1a312centroid of 12 is ( 3a/2 , 0 ) centroid of 13 is ( 0 , 2a ) centroid of 23 is ( 3a/2
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 2SolutionsQuestion 1 General shear flow distributionq= Sy t y ds I t x ds Ix 0 y0sSxsBut t ds = dA , the e
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 3Solutions6451 1 1-2 23 3-2D x1 = 023y = 120D x 2 = 9600 D x3 = 0D x12 = 1 . 120 . ds = 120s0sy = 12
Imperial College - AE - A.213
Imperial College of Science, Technology & Medicine Department of AeronauticsSecond Year Structural Mechanics and Dynamics II Tutorial Sheet 4SolutionsBa t a Bb b d For an element of the skin the contribution to the boom areas areB a = td 6 b + 2 a an
CUNY Hunter - ENGL - 220
Dorina Jaubelli English 220 Professor KoThe TempestThe Tempest is praised as one of Shakespeares finest works, one may wonder why this may be. A possible reason could be the way characters psychologically develop throughout the five acts. Specifically,
CUNY Hunter - ENGL - 220
Dorina Jaubelli Joost Burgers 12.6.2009 Cover LetterEnglish 120 has proven to be exceedingly helpful. I had a great professor who structured the class to be very practical, making the experience a positive one. The diagnostic essay helped determine which
École Normale Supérieure - ACCOUNTING - ACC202
6.checkandcite:Major League Baseball Properties (MLBP), established in 1984, controls the marketing and licensing of all league-wide and teams trademarks. In order to bind all teams to a contract, three-quarters of the teams must agree to the terms of a
A.T. Still University - PHYSICS - 2331001
TJ Physics PS 29 Due 2/25-26/2010 Note: Calculus is not required to solve these problems.1. Three charges are arranged as shown in the figure below. In unit vector notation, calculate the force on the charge at the origin. Y 5.00 nC 0.300 m 0.100 m -3.00
UNC - ART - 152
Title: Santa Maria del Fiore Cathedral (Duomo) Art Historical Period: 14th Century Art in Europe Date: plan [1250-1300], bell tower [1300-1350], drum and dome [1400-1450] Place of Execution: Florence, Italy Artist: plan by Arnolfo di Cambio, Campanile (be
UNC - ART - 152
Title: Well of Moses Art Historical Period: Medium: limestone with traces of paint Date: [1400-1450] Place of Execution: Dijon, France Artist: Claus Sluter Significance: detail of Moses and David, for the Chartreuse de ChampmolTitle: Duke of Berry at Tab
UNC - ART - 152
Title: Dome of Florence Cathedral (Duomo) Art Historical Period: Medium: Date: [1400-1450] Place of Execution: Florence, Italy Artist: Filippo Brunelleschi Significance: lantern by Michelozzo di Bartolomeo completed 1471Title: Church of San Lorenzo, Sacr
UNC - ART - 152
Title: Saint Sebastian Art Historical Period: 15th Century Italy Medium: oil on panel Date: [1450-1500] Place of Execution: Italy Artist: Pietro Perugino Significance:Title: The Last Supper Art Historical Period: Medium: tempera and oil on plaster Date:
UNC - ART - 152
Title: Shrine of Isenheim Altarpiece Art Historical Period: Medium: painted and gilt limewood Date: [1500-1550] Place of Execution: Germany Artist: Nikolaus Hagenaur Significance:Title: Isenheim Altarpiece Shutters Art Historical Period: Medium: oil on w
UNC - ART - 152
ART 152: 14th Century Art in Europe Monuments Title: Virgin and Child Enthroned Art Historical Period: 14th Century Art in Europe Medium: tempera and gold on wood panel Date: [1250-1300] Place of Execution: Florence, Italy Artist: Cimabue Significance: po
UNC - ART - 152
ART 152: Fifteenth Century Art in Northern Europe and Iberia Monuments Title: Well of Moses Art Historical Period: Medium: limestone with traces of paint Date: [1400-1450] Place of Execution: Dijon, France Artist: Claus Sluter Significance: detail of Mose
UNC - ART - 152
ART 152: Fifteenth Century Art in Italy Monuments Title: Dome of Florence Cathedral (Duomo) Art Historical Period: Medium: Date: [1400-1450] Place of Execution: Florence, Italy Artist: Filippo Brunelleschi Significance: lantern by Michelozzo di Bartolomeo