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- Mechanical Vibrations and Structural Dynamics - MVSD
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- Introduction to mechanical vibration - ( 2 - 12 )
- Vibration under Harmonic Forcing Conditions - ( 13 - 29 )
- Vibration Under General Forcing Conditions - ( 30 - 40 )
- Two and Multi - DOF System - ( 41 - 77 )
- Continuous Systems - ( 78 - 109 )
- Applications of forced vibration response analysis - ( 110 - 117 )
- Forced Response in Multiple degree-of-freedom systems - ( 118 - 131 )

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MECHANICAL VIBRATIONS AND STRUCTURAL DYNAMICS UNIT-I 1 Introduction to Mechanical Vibrations 1.1 IMPORTANCE OF VIBRATIONS Vibrations are oscillations in mechanical dynamic systems. Although any system can oscillate when it is forced to do so externally, the term “vibration” in mechanical engineering is often reserved for systems that can oscillate freely without applied forces. Sometimes these vibrations cause minor or serious performance or safety problems in engineered systems. For instance, when an aircraft wing vibrates excessively, passengers in the aircraft become uncomfortable especially when the frequencies of vibration correspond to natural frequencies of the human body and organs. In fact, it is well known that the resonant frequency of the human intestinal tract (approx. 4-8 Hz) should be avoided at all costs when designing high performance aircraft and reusable launch vehicles because sustained exposure can cause serious internal trauma (Leatherwood and Dempsey, 1976 NASA TN D-8188). If an aircraft wing vibrates at large amplitudes for an extended period of time, the wing will eventually experience a fatigue failure of some kind, which would potentially cause the aircraft to crash resulting in injuries and/or fatalities. Wing vibrations of this type are usually associated with the wide variety of flutter phenomena brought on by fluid-structure interactions. The most famous engineering disaster of all time was the Tacoma Narrows Bridge disaster in 1940 (see Figure 1.1 below). It failed due to the same type of self-excited vibration behavior that occurs in aircraft wings. Figure 1.1: (left) View of Tacoma Narrows Bridge along deck; (right) view of torsional vibration In reading books and technical papers on vibration including the previous paragraph, engineering students are usually left with the impression that all vibrations are detrimental because most publicized work discusses vibration reduction in one form or another. But

MECHANICAL VIBRATIONS AND STRUCTURAL DYNAMICS vibrations can also be beneficial. For instance, many different types of mining operations rely on sifting vibrations through which different sized particles are sorted using vibrations. In nature, vibrations are also used by all kinds of different species in their daily lives. Orb web spiders, for example, use vibrations in their webs to detect the presence of flies and other insects as they struggle after being captured in the web for food. The reason that mechanical systems vibrate freely is because energy is exchanged between the system’s inertial (masses) elements and elastic (springs) elements. Free vibrations usually cease after a certain length of time because damping elements in systems dissipate energy as it is converted back-and-forth between kinetic energy and potential energy. The role of mechanical vibration analysis should be to use mathematical tools for modeling and predicting potential vibration problems and solutions, which are usually not obvious in preliminary engineering designs. If problems can be predicted, then designs can be modified to mitigate vibration problems before systems are manufactured. Vibrations can also be intentionally introduced into designs to take advantage of benefits of relative mechanical motion and to resonate systems (e.g., scanning microscopy). Unfortunately, knowledge of vibrations in preliminary mechanical designs is rarely considered essential, so many vibration studies are carried out only after systems are manufactured. In these cases, vibration problems must be addressed using passive or active design modifications. Sometimes a design modification may be as simple as a thickness change in a vibrating panel; added thickness tends to push the resonant frequencies of a panel higher leading to less vibration in the operating frequency range. Design modifications can also be as complicated as inserting magneto-rheological (MR) fluid dampers into mechanical systems to take energy away from vibrating systems at specific times during their motion. The point here is that design changes prior to manufacture are less expensive and more effective than design modifications done later on. 1.2 Modeling issues Modeling is usually 95% of the effort in real-world mechanical vibration problems; however, this course will focus primarily on the derivation of equations of motion, free response and forced response analysis, and approximate solution methods for vibrating systems. Figure 1.2 illustrates one example of why modeling can be challenging in mechanical vibrating systems. A large crane on a shipping dock is shown loading/unloading packages from a cargo ship. In one possible vibration scenario, the cable might be idealized as massless and the crane idealized as rigid. In

MECHANICAL VIBRATIONS AND STRUCTURAL DYNAMICS this simple case, the package and crane both oscillate as rigid bodies; the package oscillates about the end of the crane and the crane oscillates about its base point of rotation as the two exchange energy. These vibrations would most likely correspond to relatively low frequencies and would take place in addition to the gross dynamical motion of the crane and package. Two coupled ordinary differential equations would be needed in this case to model the discrete, independent motions of the crane and package. This model might be sufficient in some cases, but what if the mass of the cable is comparable to the mass of the package? In this case, the crane and package still behave like rigid bodies, but the cable will probably vibrate either transversely or longitudinally as a continuous body along its length. These higher frequency vibrations would require that both ordinary differential equations for the crane and package and partial differential equations of the cable be used to model the entire system. Furthermore, if the assumption of rigidity in the crane were also relaxed, then it too would need to be modeled with partial differential equations. All of these complications would be superimposed on top of the simple rigid body dynamics of the crane and package. Figure 1.2: Crane for loading/unloading packages from cargo ship. Different regimes of operation require different levels of sophistication in the mechanical vibration model. We will have the opportunity to discuss modeling considerations throughout the course when case studies of vibration phenomena are used to reinforce theoretical concepts and analysis procedures. Before starting to analyze systems, we must be able to derive differential equations 1-4

MECHANICAL VIBRATIONS AND STRUCTURAL DYNAMICS of motion that adequately describe the systems. There are many different methods for doing this; these are discussed in Chapter 2. 1.3 Linear superposition as a “working” principle We cannot discuss everything in this course. In particular, there is not sufficient time to present linear and nonlinear methods of vibration analysis. Therefore, the course will primarily focus on linear vibrating systems and linear approaches to analysis. Only certain special characteristics of nonlinear systems will be introduced during the semester. Because the decision has been made to talk primarily about linear systems, the principle of superposition will hold in every problem that is discussed. Instead of stating this principle at the beginning of the course, and referencing it when it is needed in proofs and derivations, we will view it more as a “working” principle. In other words, linear superposition will guide us in our analysis of free and forced linear vibrations. When we begin to analyze vibrations, we will look to the principle of superposition to help us move forward in our analyses. Recall that a mathematical operator, L[], which obeys the principle of linear superposition by definition satisfies the following two expressions: ( 1.1 ) and ( 1.2 ) where L is said to operate on the two different functions, x and y, and a and b are constants. Eq. ( 1.1 ) is the principle of homogeneity and Eq. ( 1.2 ) is the principle of additivity. These two expressions may seem trivial or obvious, but they will in fact be extraordinarily useful later in the course. The important point to remember is that linear systems, which are governed by linear operators, L[], are equal to the sum of their parts. Although this statement is profound and may even be fruit for philosophical discussions, the motivation for putting linear vibration into the context of linear superposition here is that it makes vibration analysis in free and forced systems much easier to develop and understand. More will be said about superposition in Chapter 3. 1-5

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