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32.9.1 Engineering Stress-Strain Traditionally, the tensile test has been used to determine the so-called engineering stress-strain data that are needed to plot the engineering stress-strain curve for a given material. However, since engineering stress is not really a stress but is a mea-

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four switch inputs, software-controlled backlight, custom characters, and buzzer output. The data output of the AM-HRR3 on pin 14 is fed directly to the serial ILM-216L display. The ILM-216L display unit provides 8 pins for interfacing. Pins 1 and 6 are tied to ground, and 5 Vdc is applied to pin 2 to power the display. Serial data input is applied to pin 3, while data output from the display is provided on pin 4. A piezo alarm buzzer can be connected to pin 5. The baud rate can be changed via pin 8, using the configuration/test input on pin 7. The receiver is coupled directly to serial input on pin 3 of the display. The receiver and display are both powered from the 5-V regulator at U1. A piezo buzzer is connected to pin 5 of the display unit to provide an audible indication that an alarm condition has occurred. In operation, once the alarm controller is triggered, the STAMP 2 sends out serial data through the transmitter to the receiver at RX. The STAMP 2 sends out a serial word to activate the buzzer three times to get your attention; you can modify the program to preset a longer alarm sound if desired. Once the buzzer has been activated, the STAMP 2 begins sending out a serial data message to the LCD display unit, which indicates which alarm channel has been activated. The transmitter and receiver combination will operate up to 3 kHz, so the serial data stream from the STAMP 2 to the transmitter was set up to 2400 baud. Note that by using the Abacom FM transmitter/receiver pair the system is capable of 9600-baud operation.

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sure of the strength of a material, it is more appropriate to call such data either strength nominal strain or nominal stress strain data. Table 32.3 illustrates the data that are normally collected during a tensile test, and Fig. 32.14 shows the condition of a standard tensile specimen at the time the specific data in the table are recorded. The load-versus-gauge-length data, or an elastic stress-strain curve drawn by the machine, are needed to determine Young s modulus of elasticity of the material as well as the proportional limit. They are also needed to determine the yield strength if the offset method is used. All the definitions associated with engineering stressstrain, or, more appropriately, with the strength nominal strain properties, are presented in the section which follows and are discussed in conjunction with the experimental data for commercially pure titanium listed in Table 32.3 and Fig. 32.14. The elastic and elastic-plastic data listed in Table 32.3 are plotted in Fig. 32.15 with an expanded strain axis, which is necessary for the determination of the yield strength. The nominal (approximate) stress or the strength S which is calculated by means of Eq. (32.8) is plotted as the ordinate. The abscissa of the engineering stress-strain plot is the nominal strain, which is defined as the unit elongation obtained when the change in length is divided by the original length and has the units of inch per inch and is designated as n. Thus, for tension, n= =

(32.10)

where = gauge length and the subscripts 0 and f designate the original and final state, respectively. This equation is valid for deformation strains that do not exceed the strain at the maximum load of a tensile specimen. It is customary to plot the data obtained from a tensile test as a stress-strain curve such as that illustrated in Fig. 32.16, but without including the word nominal. The reader then considers such a curve as an actual stress-strain curve, which it obviously is not. The curve plotted in Fig. 32.16 is in reality a load-deformation curve. If the ordinate axis were labeled load (lb) rather than stress (psi), the distinction between

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