NLR rapport Memo VV-70-005 d.d. 19 februari 1970. Remarks on the Northrop/AETE flight-test-programme to demonstrate accuracy of the NF-5A doppler navigation system. NLR rapport TR 72100 C d.d. 7-8-1972. Calibration of NF-5A K-3001 test nose boom and verification of angle of attack data provided by Northrop. NLR rapport TR 74112 C d.d. 15-8-1974. A tentative fatigue test load history for fighter aircraft. 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 MP 79008 U d.d. 23-2-1979. Re-assesment of service life by comparative specimen tests. NLR rapport Memorandum WE-80-16 C d.d. 17-03-1980. Delivery and impact analysis system-DIAS environmental test report; camera and control electronics. NLR rapport TR 82098 C d.d. 25-9-1982. Description of a database containing measured load distributions in the wing of the NF-5A test aircraft (K-3001). NLR rapport AA.323 d.d. onbekend ± 1950/60. Pressure-plotting measurements on a wing with variable sweep and aspect ratio and with blowing over the flaps and … NLL Verslagen en verhandelingen XVIII - 1953. A.1205. The field of flow through a helicopter rotor obtained from windtunnel smoke tests. NLL Verslagen en verhandelingen XVIII - 1953. S. 416. Comparative fatigue tests with 24 ST Alclad rivited and bonded stiffenend panels. NLL Verslagen en verhandelingen XVIII - 1953. S. 421. Torsional strength and stiffness tests on wing leading edges.
