Rigid Bodies; Equivalent Systems of Forces
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The Experimental Determination of the Moment of Inertia of a Model Airplane Michael Koken [email protected]
The University of Akron IdeaExchange@UAkron The Dr. Gary B. and Pamela S. Williams Honors Honors Research Projects College Fall 2017 The Experimental Determination of the Moment of Inertia of a Model Airplane Michael Koken [email protected] Please take a moment to share how this work helps you through this survey. Your feedback will be important as we plan further development of our repository. Follow this and additional works at: http://ideaexchange.uakron.edu/honors_research_projects Part of the Aerospace Engineering Commons, Aviation Commons, Civil and Environmental Engineering Commons, Mechanical Engineering Commons, and the Physics Commons Recommended Citation Koken, Michael, "The Experimental Determination of the Moment of Inertia of a Model Airplane" (2017). Honors Research Projects. 585. http://ideaexchange.uakron.edu/honors_research_projects/585 This Honors Research Project is brought to you for free and open access by The Dr. Gary B. and Pamela S. Williams Honors College at IdeaExchange@UAkron, the institutional repository of The nivU ersity of Akron in Akron, Ohio, USA. It has been accepted for inclusion in Honors Research Projects by an authorized administrator of IdeaExchange@UAkron. For more information, please contact [email protected], [email protected]. 2017 THE EXPERIMENTAL DETERMINATION OF A MODEL AIRPLANE KOKEN, MICHAEL THE UNIVERSITY OF AKRON Honors Project TABLE OF CONTENTS List of Tables ................................................................................................................................................ -
Rotational Motion (The Dynamics of a Rigid Body)
University of Nebraska - Lincoln DigitalCommons@University of Nebraska - Lincoln Robert Katz Publications Research Papers in Physics and Astronomy 1-1958 Physics, Chapter 11: Rotational Motion (The Dynamics of a Rigid Body) Henry Semat City College of New York Robert Katz University of Nebraska-Lincoln, [email protected] Follow this and additional works at: https://digitalcommons.unl.edu/physicskatz Part of the Physics Commons Semat, Henry and Katz, Robert, "Physics, Chapter 11: Rotational Motion (The Dynamics of a Rigid Body)" (1958). Robert Katz Publications. 141. https://digitalcommons.unl.edu/physicskatz/141 This Article is brought to you for free and open access by the Research Papers in Physics and Astronomy at DigitalCommons@University of Nebraska - Lincoln. It has been accepted for inclusion in Robert Katz Publications by an authorized administrator of DigitalCommons@University of Nebraska - Lincoln. 11 Rotational Motion (The Dynamics of a Rigid Body) 11-1 Motion about a Fixed Axis The motion of the flywheel of an engine and of a pulley on its axle are examples of an important type of motion of a rigid body, that of the motion of rotation about a fixed axis. Consider the motion of a uniform disk rotat ing about a fixed axis passing through its center of gravity C perpendicular to the face of the disk, as shown in Figure 11-1. The motion of this disk may be de scribed in terms of the motions of each of its individual particles, but a better way to describe the motion is in terms of the angle through which the disk rotates. -
Pierre Simon Laplace - Biography Paper
Pierre Simon Laplace - Biography Paper MATH 4010 Melissa R. Moore University of Colorado- Denver April 1, 2008 2 Many people contributed to the scientific fields of mathematics, physics, chemistry and astronomy. According to Gillispie (1997), Pierre Simon Laplace was the most influential scientist in all history, (p.vii). Laplace helped form the modern scientific disciplines. His techniques are used diligently by engineers, mathematicians and physicists. His diverse collection of work ranged in all fields but began in mathematics. Laplace was born in Normandy in 1749. His father, Pierre, was a syndic of a parish and his mother, Marie-Anne, was from a family of farmers. Many accounts refer to Laplace as a peasant. While it was not exactly known the profession of his Uncle Louis, priest, mathematician or teacher, speculations implied he was an educated man. In 1756, Laplace enrolled at the Beaumont-en-Auge, a secondary school run the Benedictine order. He studied there until the age of sixteen. The nest step of education led to either the army or the church. His father intended him for ecclesiastical vocation, according to Gillispie (1997 p.3). In 1766, Laplace went to the University of Caen to begin preparation for a career in the church, according to Katz (1998 p.609). Cristophe Gadbled and Pierre Le Canu taught Laplace mathematics, which in turn showed him his talents. In 1768, Laplace left for Paris to pursue mathematics further. Le Canu gave Laplace a letter of recommendation to d’Alembert, according to Gillispie (1997 p.3). Allegedly d’Alembert gave Laplace a problem which he solved immediately. -
Magnetism, Angular Momentum, and Spin
Chapter 19 Magnetism, Angular Momentum, and Spin P. J. Grandinetti Chem. 4300 P. J. Grandinetti Chapter 19: Magnetism, Angular Momentum, and Spin In 1820 Hans Christian Ørsted discovered that electric current produces a magnetic field that deflects compass needle from magnetic north, establishing first direct connection between fields of electricity and magnetism. P. J. Grandinetti Chapter 19: Magnetism, Angular Momentum, and Spin Biot-Savart Law Jean-Baptiste Biot and Félix Savart worked out that magnetic field, B⃗, produced at distance r away from section of wire of length dl carrying steady current I is 휇 I d⃗l × ⃗r dB⃗ = 0 Biot-Savart law 4휋 r3 Direction of magnetic field vector is given by “right-hand” rule: if you point thumb of your right hand along direction of current then your fingers will curl in direction of magnetic field. current P. J. Grandinetti Chapter 19: Magnetism, Angular Momentum, and Spin Microscopic Origins of Magnetism Shortly after Biot and Savart, Ampére suggested that magnetism in matter arises from a multitude of ring currents circulating at atomic and molecular scale. André-Marie Ampére 1775 - 1836 P. J. Grandinetti Chapter 19: Magnetism, Angular Momentum, and Spin Magnetic dipole moment from current loop Current flowing in flat loop of wire with area A will generate magnetic field magnetic which, at distance much larger than radius, r, appears identical to field dipole produced by point magnetic dipole with strength of radius 휇 = | ⃗휇| = I ⋅ A current Example What is magnetic dipole moment induced by e* in circular orbit of radius r with linear velocity v? * 휋 Solution: For e with linear velocity of v the time for one orbit is torbit = 2 r_v. -
Statics FE Review 032712.Pptx
FE Stacs Review h0p://www.coe.utah.edu/current-undergrad/fee.php Scroll down to: Stacs Review - Slides Torch Ellio [email protected] (801) 587-9016 MCE room 2016 (through 2000B door) Posi'on and Unit Vectors Y If you wanted to express a 100 lb force that was in the direction from A to B in (-2,6,3). A vector form, then you would find eAB and multiply it by 100 lb. rAB O x rAB = 7i - 7j – k (units of length) B .(5,-1,2) e = (7i-7j–k)/sqrt[99] (unitless) AB z Then: F = F eAB F = 100 lb {(7i-7j–k)/sqrt[99]} Another Way to Define a Unit Vectors Y Direction Cosines The θ values are the angles from the F coordinate axes to the vector F. The θY cosines of these θ values are the O θx x θz coefficients of the unit vector in the direction of F. z If cos(θx) = 0.500, cos(θy) = 0.643, and cos(θz) = - 0.580, then: F = F (0.500i + 0.643j – 0.580k) TrigonometrY hYpotenuse opposite right triangle θ adjacent • Sin θ = opposite/hYpotenuse • Cos θ = adjacent/hYpotenuse • Tan θ = opposite/adjacent TrigonometrY Con'nued A c B anY triangle b C a Σangles = a + b + c = 180o Law of sines: (sin a)/A = (sin b)/B = (sin c)/C Law of cosines: C2 = A2 + B2 – 2AB(cos c) Products of Vectors – Dot Product U . V = UVcos(θ) for 0 <= θ <= 180ο ( This is a scalar.) U In Cartesian coordinates: θ . -
Rigid Body Dynamics 2
Rigid Body Dynamics 2 CSE169: Computer Animation Instructor: Steve Rotenberg UCSD, Winter 2017 Cross Product & Hat Operator Derivative of a Rotating Vector Let’s say that vector r is rotating around the origin, maintaining a fixed distance At any instant, it has an angular velocity of ω ω dr r ω r dt ω r Product Rule The product rule of differential calculus can be extended to vector and matrix products as well da b da db b a dt dt dt dab da db b a dt dt dt dA B dA dB B A dt dt dt Rigid Bodies We treat a rigid body as a system of particles, where the distance between any two particles is fixed We will assume that internal forces are generated to hold the relative positions fixed. These internal forces are all balanced out with Newton’s third law, so that they all cancel out and have no effect on the total momentum or angular momentum The rigid body can actually have an infinite number of particles, spread out over a finite volume Instead of mass being concentrated at discrete points, we will consider the density as being variable over the volume Rigid Body Mass With a system of particles, we defined the total mass as: n m m i i1 For a rigid body, we will define it as the integral of the density ρ over some volumetric domain Ω m d Angular Momentum The linear momentum of a particle is 퐩 = 푚퐯 We define the moment of momentum (or angular momentum) of a particle at some offset r as the vector 퐋 = 퐫 × 퐩 Like linear momentum, angular momentum is conserved in a mechanical system If the particle is constrained only -
Finite Element Model Calibration of an Instrumented Thirteen-Story Steel Moment Frame Building in South San Fernando Valley, California
Finite Element Model Calibration of An Instrumented Thirteen-story Steel Moment Frame Building in South San Fernando Valley, California By Erol Kalkan Disclamer The finite element model incuding its executable file are provided by the copyright holder "as is" and any express or implied warranties, including, but not limited to, the implied warranties of merchantability and fitness for a particular purpose are disclaimed. In no event shall the copyright owner be liable for any direct, indirect, incidental, special, exemplary, or consequential damages (including, but not limited to, procurement of substitute goods or services; loss of use, data, or profits; or business interruption) however caused and on any theory of liability, whether in contract, strict liability, or tort (including negligence or otherwise) arising in any way out of the use of this software, even if advised of the possibility of such damage. Acknowledgments Ground motions were recorded at a station owned and maintained by the California Geological Survey (CGS). Data can be downloaded from CESMD Virtual Data Center at: http://www.strongmotioncenter.org/cgi-bin/CESMD/StaEvent.pl?stacode=CE24567. Contents Introduction ..................................................................................................................................................... 1 OpenSEES Model ........................................................................................................................................... 3 Calibration of OpenSEES Model to Observed Response -
Rigid Body Dynamics II
An Introduction to Physically Based Modeling: Rigid Body Simulation IIÐNonpenetration Constraints David Baraff Robotics Institute Carnegie Mellon University Please note: This document is 1997 by David Baraff. This chapter may be freely duplicated and distributed so long as no consideration is received in return, and this copyright notice remains intact. Part II. Nonpenetration Constraints 6 Problems of Nonpenetration Constraints Now that we know how to write and implement the equations of motion for a rigid body, let's consider the problem of preventing bodies from inter-penetrating as they move about an environment. For simplicity, suppose we simulate dropping a point mass (i.e. a single particle) onto a ®xed ¯oor. There are several issues involved here. Because we are dealing with rigid bodies, that are totally non-¯exible, we don't want to allow any inter-penetration at all when the particle strikes the ¯oor. (If we considered our ¯oor to be ¯exible, we might allow the particle to inter-penetrate some small distance, and view that as the ¯oor actually deforming near where the particle impacted. But we don't consider the ¯oor to be ¯exible, so we don't want any inter-penetration at all.) This means that at the instant that the particle actually comes into contact with the ¯oor, what we would like is to abruptly change the velocity of the particle. This is quite different from the approach taken for ¯exible bodies. For a ¯exible body, say a rubber ball, we might consider the collision as occurring gradually. That is, over some fairly small, but non-zero span of time, a force would act between the ball and the ¯oor and change the ball's velocity. -
Rotation: Moment of Inertia and Torque
Rotation: Moment of Inertia and Torque Every time we push a door open or tighten a bolt using a wrench, we apply a force that results in a rotational motion about a fixed axis. Through experience we learn that where the force is applied and how the force is applied is just as important as how much force is applied when we want to make something rotate. This tutorial discusses the dynamics of an object rotating about a fixed axis and introduces the concepts of torque and moment of inertia. These concepts allows us to get a better understanding of why pushing a door towards its hinges is not very a very effective way to make it open, why using a longer wrench makes it easier to loosen a tight bolt, etc. This module begins by looking at the kinetic energy of rotation and by defining a quantity known as the moment of inertia which is the rotational analog of mass. Then it proceeds to discuss the quantity called torque which is the rotational analog of force and is the physical quantity that is required to changed an object's state of rotational motion. Moment of Inertia Kinetic Energy of Rotation Consider a rigid object rotating about a fixed axis at a certain angular velocity. Since every particle in the object is moving, every particle has kinetic energy. To find the total kinetic energy related to the rotation of the body, the sum of the kinetic energy of every particle due to the rotational motion is taken. The total kinetic energy can be expressed as .. -
Twisting Couple on a Cylinder Or Wire
Course: US01CPHY01 UNIT – 2 ELASTICITY – II Introduction: We discussed fundamental concept of properties of matter in first unit. This concept will be more use full for calculating various properties of mechanics of solid material. In this unit, we shall study the detail theory and its related experimental methods for determination of elastic constants and other related properties. Twisting couple on a cylinder or wire: Consider a cylindrical rod of length l radius r and coefficient of rigidity . Its upper end is fixed and a couple is applied in a plane perpendicular to its length at lower end as shown in fig.(a) Consider a cylinder is consisting a large number of co-axial hollow cylinder. Now, consider a one hollow cylinder of radius x and radial thickness dx as shown in fig.(b). Let is the twisting angle. The displacement is greatest at the rim and decreases as the center is approached where it becomes zero. As shown in fig.(a), Let AB be the line parallel to the axis OO’ before twist produced and on twisted B shifts to B’, then line AB become AB’. Before twisting if hollow cylinder cut along AB and flatted out, it will form the rectangular ABCD as shown in fig.(c). But if it will be cut after twisting it takes the shape of a parallelogram AB’C’D. The angle of shear From fig.(c) ∠ ̼̻̼′ = ∅ From fig.(b) ɑ ̼̼ = ͠∅ ɑ BB = xθ ∴ ͠∅ = ͬ Page 1 of 20 ͬ ∴ ∅ = … … … … … … (1) The modules of͠ rigidity is ͍ℎ͙͕ͦ͛͢͝ ͙ͧͤͦͧͧ ̀ = = ͕͙͛͢͠ ͚ͣ ͧℎ͙͕ͦ & ͬ ∴ ̀ = ∙ ∅ = The surface area of this hollow cylinder͠ = 2ͬͬ͘ Total shearing force on this area ∴ ͬ = 2ͬͬ͘ ∙ ͠ ͦ The moment of this force= 2 ͬ ͬ͘ ͠ ͦ = 2 ͬ ͬ͘ ∙ ͬ ͠ 2 ͧ Now, integrating between= theͬ limits∙ ͬ͘ x = 0 and x = r, We have, total twisting couple͠ on the cylinder - 2 ͧ = ǹ ͬ ͬ͘ * ͠ - 2 ͧ = ǹ ͬ ͬ͘ ͠ * ͨ - 2 ͬ = ʨ ʩ Total twisting couple ͠ 4 * ∴ ͨ ͦ = … … … … … … (3) Then, the twisting couple2͠ per unit twist ( ) is = 1 ͨ ͦ ̽ = … … … … … … (4) This twisting couple per unit twist 2͠is also called the torsional rigidity of the cylinder or wire. -
Total Angular Momentum
Total Angular momentum Dipanjan Mazumdar Sept 2019 1 Motivation So far, somewhat deliberately, in our prior examples we have worked exclusively with the spin angular momentum and ignored the orbital component. This is acceptable for L = 0 systems such as filled shell atoms, but properties of partially filled atoms will depend both on the orbital and the spin part of the angular momentum. Also, when we include relativistic corrections to atomic Hamiltonian, both spin and orbital angular momentum enter directly through terms like L:~ S~ called the spin-orbit coupling. So instead of focusing only on the spin or orbital angular momentum, we have to develop an understanding as to how they couple together. One of the ways is through the total angular momentum defined as J~ = L~ + S~ (1) We will see that this will be very useful in many cases such as the real hydrogen atom where the eigenstates after including the fine structure effects such as spin-orbit interaction are eigenstates of the total angular momentum operator. 2 Vector model of angular momentum Let us first develop an intuitive understanding of the total angular momentum through the vector model which is a semi-classical approach to \add" angular momenta using vector algebra. We shall first ask, knowing L~ and S~, what are the maxmimum and minimum values of J^. This is simple to answer us- ing the vector model since vectors can be added or subtracted. Therefore, the extreme values are L~ + S~ and L~ − S~ as seen in figure 1.1 Therefore, the total angular momentum will take up values between l+s Figure 1: Maximum and minimum values of angular and jl − sj. -
Fundamental Governing Equations of Motion in Consistent Continuum Mechanics
Fundamental governing equations of motion in consistent continuum mechanics Ali R. Hadjesfandiari, Gary F. Dargush Department of Mechanical and Aerospace Engineering University at Buffalo, The State University of New York, Buffalo, NY 14260 USA [email protected], [email protected] October 1, 2018 Abstract We investigate the consistency of the fundamental governing equations of motion in continuum mechanics. In the first step, we examine the governing equations for a system of particles, which can be considered as the discrete analog of the continuum. Based on Newton’s third law of action and reaction, there are two vectorial governing equations of motion for a system of particles, the force and moment equations. As is well known, these equations provide the governing equations of motion for infinitesimal elements of matter at each point, consisting of three force equations for translation, and three moment equations for rotation. We also examine the character of other first and second moment equations, which result in non-physical governing equations violating Newton’s third law of action and reaction. Finally, we derive the consistent governing equations of motion in continuum mechanics within the framework of couple stress theory. For completeness, the original couple stress theory and its evolution toward consistent couple stress theory are presented in true tensorial forms. Keywords: Governing equations of motion, Higher moment equations, Couple stress theory, Third order tensors, Newton’s third law of action and reaction 1 1. Introduction The governing equations of motion in continuum mechanics are based on the governing equations for systems of particles, in which the effect of internal forces are cancelled based on Newton’s third law of action and reaction.