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-76-002 d.d. 13-1-1976. Investigations on fin loads for NF-5A/B. (2 exemplaren) NLR rapport TR 76019 C d.d. 13-2-1976. Summary report NF-5A multiparameter usage recordings. NLR rapport SB-76-034 d.d. 1-3-1976. NF-5A/B wing structure; fatigue program status and projected activities. NLR rapport SB-76-035 d.d. 1-3-1976. NF-5A/B vertical tail 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. NLR rapport Memorandum SC-77-172 d.d. 21-12-1977. Comparison of measured and calculated strains near the critical radius in the vertical tail of the NF-5A. NLR rapport TR 79008 C d.d. januari 1977. Investigation of the load distribution in the NF-5A vertical tail section and of the stress in the …
