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 … NLR rapport TR 74112 C d.d. 15-8-1974. A tentative fatigue test load history for fighter aircraft. 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 TR 76019 C d.d. 13-2-1976. Summary report NF-5A multiparameter usage recordings. 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 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 … NLR rapport Memorandum VG-79-017 C d.d. 30 april 1979. Handleiding voor het opmeten van target- en vliegtuig-referentiepunten en de openingshoeken van een fotocamera t.b.v. DIAS.
