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. NLL Verslagen en verhandelingen XX1 - 1959. TR F.206. Linearized theory of lifting sweptback wings at sonic speed. NLR Verslagen en verhandelingen XXV - 1961. TR S.578. On the analysis of swept wing structures. NLR Verslagen en verhandelingen XXVIII - 1964. TR G.6. The complete solution for the problem of a ring wing around a circular cylindrical fuselage in … NLR Verslagen en verhandelingen XXX - 1965. TR W.7. Tunnel wall corrections for a wing-flap system between two parallel walls. NLR Verslagen en verhandelingen XXX - 1965. TR W.8. Two-dimensional tunnel wall corrections for a wing with a blown flap between two parallel walls.
