Design and evaluation of a bolted joint for a discrete carbon-epoxy rod-reinforced hat section

Original publisher: Hampton, Va.: National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va.: National Technical Information Service, distributor, 1996] OCLC Number: ocm37955926 Excerpt: ... Figure 14.-Location of strain gages on compression test specimen. Figure 15.-Strain gage results at location Figure 16.-Strain gage results at between bolts 209 and 210 centerline of specimen. ( see figure 8 ). 14