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The effect of static tensile load on the thermal expansion of Gr/PI composite material was measured for seven different laminate configurations. A computer program was developed which implements laminate theory in a piecewise linear fashion to predict the coupled nonlinear thermomechanical behavior. Static tensile load significantly affected the thermal expansion characteristics of the laminates tested. This effect is attributed to a fiber instability micromechanical behavior of the constituent materials. Analytical results correlated reasonably well with free thermal expansion tests (no load applied to the specimen). However, correlation was poor for tests with an applied load. Farley, G. L. Langley Research Center NASA-TP-1867, AVRADCOM-TR-81-B-2, L-14012 DA PROJ. 1L1-61102-AH-45...
Zakup książki
Effects of Static Tensile Load on the Thermal Expansion of Gr/Pi Composite Material, National Aeronautics and Space Administration
- Język
- Rok wydania
- 2018
- Oprawa
- (miękka)
Metody płatności
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- Tytuł
- Effects of Static Tensile Load on the Thermal Expansion of Gr/Pi Composite Material
- Rok wydania
- 2018
- Oprawa
- miękka
- Liczba stron
- 38
- ISBN10
- 1725560178
- ISBN13
- 9781725560178
- Seria
- Kategorie
- Tagi
- Badania naukowe, Inżynieria, NASA
- Opis
- The effect of static tensile load on the thermal expansion of Gr/PI composite material was measured for seven different laminate configurations. A computer program was developed which implements laminate theory in a piecewise linear fashion to predict the coupled nonlinear thermomechanical behavior. Static tensile load significantly affected the thermal expansion characteristics of the laminates tested. This effect is attributed to a fiber instability micromechanical behavior of the constituent materials. Analytical results correlated reasonably well with free thermal expansion tests (no load applied to the specimen). However, correlation was poor for tests with an applied load. Farley, G. L. Langley Research Center NASA-TP-1867, AVRADCOM-TR-81-B-2, L-14012 DA PROJ. 1L1-61102-AH-45...