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. NLR Verslagen en verhandelingen XXXVI - 1970. TR F.261. On a kernel-function method for the calculation of the pressure distribution on a two-dimensional wing with … NLR Verslagen en verhandelingen XXXVI - 1970. TR G.50. Computer application of a linearised supersonic lifting surface theory on a certain class of wings.
