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. NLR Verslagen en verhandelingen XXXVI - 1970. TR 68069U. Binary flutter calculations with theoretical and empirical aerodynamic derivatives for a wing-control surface system in two-dimensional … TD-766 Fokker C.X Kopie schets AdV: plaatsing bracket voor aileronbesturingshefboom bij Bracket, upper wing rear spar, baldaquin (RH) Detail voor schets TD-329 TD-422-15ao Kopie van tek. Nr. C 16091; Reinforcements lower wing front spar, deel van C15844 TD-422-15ap Kopie van tek. Nr. C 16281; LH lower wing, rib 8, deel van C15844 TD-422-15aq Kopie van tek. Nr. C 16280; LH lower wing rib 7, deel van C15844 TD-422-15aq Kopie van tek. Nr. C 16282; LH lower wing rib 9, deel van C15844 TD-422-15as Kopie van tek. Nr. C 16283; LH lower wing rib 10, deel van C15844
