The Practice of Engineering Dynamics. Ronald J. Anderson

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part presents a logical progression of analysis techniques and methods applied to the governing equations of motion for systems. The progression is from equilibrium solutions that find in what states the system would like to be, to analyzing the stability of these equilibrium states (stability is usually considered only in textbooks on control systems but it is vitally important to dynamic systems), to considering small motions about the stable equilibrium states (this topic is covered in textbooks on vibrations but is, again, vital to engineers doing dynamic analysis), to frequency domain analysis (vibrations again), and finally to time domain solutions (these are rarely covered in textbooks).

      Part 3. Working with Experimental Data

      While not usually considered a part of the design process, analysis of experimental data measured on dynamic systems is critical to creating a successful product. To assist engineers in developing capabilities in this area, part 3 covers the practical use of discrete fourier transforms in analyzing experimental data.

      In order to emphasize the idea that any dynamic mechanical system can be analyzed using the sequence of steps presented here, all the exercises at the ends of the chapters are based on 23 mechanical systems defined in an appendix. Any one of these systems could be used as an example of all of the types of dynamic analysis.

      November, 2019

       Ronald J. Anderson Kingston, Canada

      This book is accompanied by a companion website:

       www.wiley.com/go/anderson/engineeringdynamics

      The website includes:

       Animations

       Fully worked examples

       Software

      Scan this QR code to visit the companion website.

Part I Modeling: Deriving Equations of Motion

      Vectors have two distinct properties – magnitude and direction. Either or both of these properties may change with time and the time derivative of a vector must account for both.

      The rate of change of a vector

with respect to time is therefore formed from,

      1 The rate of change of magnitude .

      2 The rate of change of direction .

that changes after a time increment,
, to
.

      The difference between

and
can be defined as the vector
shown in Figure 1.1 and, by the rules of vector addition,

      (1.1)

      or,

      (1.2)

      Then, using the definition of the time derivative,

      Imagine now that Figure 1.1 is compressed to show only an infinitesimally small time interval,

. The components of
for the interval
are shown in Figure 1.1. They are,

      1 A component aligned with the vector . This is a component that is strictly due to the rate of change of magnitude of . The magnitude of is where is the rate of change of length (or magnitude) of the vector . The direction of is the same as the direction of . Let be designated1 as .

      2 A component that is perpendicular to the vector . That is, a component due to the rate of change of direction of the vector. Terms of this type arise only when there is an angular velocity. The rate of change of direction term arises from the time rate of change of the angle in Figure 1.1 and is the magnitude of the angular velocity of the vector. The rate of change of direction therefore arises from the angular velocity of the vector. The magnitude of is where is the length of . By definition the rate of change of the angle (i.e. ) has the same positive sense as the angle itself. It is clear that is the “tip speed” one would expect from an object of length rotating with angular speed .

      The angular velocity is itself a vector quantity since it must specify both the angular

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