NLR rapport SC-71-22 d.d. 15-3-1971. Report on the instrumentation of an NF-5A wing for the Royal Netherlands Air Force, at Canadair. NLR rapport TR 74030 C d.d. 18-2-1974. Stress changes measured during the loosening of the skins from attach ribs, wing to fuselage, of the NF5 … TD-206 NLR rapport TR 75083 C d.d. mei 1975. Investigation into the cause of cracking of NF-5 wing root ribs. TD-207 NLR rapport TR 75088 C d.d. juni 1975. Stress changes measured during the mounting of new attach ribs, wing to fuselage, of the NF-5 … NLR rapport SB-76-034 d.d. 1-3-1976. NF-5A/B wing structure; fatigue program status and projected activities. TD-212 NLR rapport TR 76049 C d.d. 5-5-1976. Fractographic investigation of a cracked NF-5 wing root rib. NLR rapport TR 76080 C part I d.d. 9-9-1976. The calibration of the RNLAF NF-5A instrumented wing; Part I: Description and results. NLR rapport TR 76080 C part II d.d. 9-9-1976. The calibration of the RNLAF NF-5A instrumented wing; Part II: Influence coefficient plots. TD-215 NLR rapport TR 76115 C d.d. 9-9-1976. Development of fatigue test specimen for the NF-5 wing lower skin. TD-216 NLR rapport TR 77088 C d.d. 29-7-1977. Flight load tests on NF-5 wing skin specimens. TD-223 NLR rapport TR 80003 C d.d. 8-7-1980. Stress changes in flanges of new attach ribs caused by assembly, mounting and setting of the NF-5 … TD-225 NLR rapport TR 80028 C d.d. 18-3-1980. Investigation of a cracked NF-5 wing root rib.
