NASA NTRS · 19810022685
National Transonic Facility Fan Blade prepreg material characterization tests
Abstract
The test program for the basic prepreg materials used in process development work and planned fabrication of the national transonic facility fan blade is presented. The basic prepreg materials and the design laminate are characterized at 89 K, room temperature, and 366 K. Characterization tests, test equipment, and test data are discussed. Material tests results in the warp direction are given for tensile, compressive, fatigue (tension-tension), interlaminar shear and thermal expansion.
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Klich, P. J., Richards, W. H., Ahl, E. L., Jr.. 1981-07-01. National Transonic Facility Fan Blade prepreg material characterization tests. https://ntrs.nasa.gov/citations/19810022685
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