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. 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 rapport W.7 d.d. 5-4-1961. Tunnelwall corrections for a wing-flap system between two parallel walls. NLR rapport W.8 d.d. 15-10-1961. Two-dimensional tunnelwall corrections for a wing with a blown flap between two parallel walls. NLL Verslagen en verhandelingen XVIII - 1953. F.118. Influence of compressibility on the calculated flexure-torsion flutter speed of a family of rectangular cantilever wings. NLL Verslagen en verhandelingen XVIII - 1953. S. 421. Torsional strength and stiffness tests on wing leading edges. NLL Verslagen en verhandelingen XX1 - 1959. TN F.192. Calculation of aerodynamic forces on slowly oscillating rectangular wings in subsonic flow.
