NLL Verslagen en verhandelingen XVIII - 1953. S. 416. Comparative fatigue tests with 24 ST Alclad rivited and bonded stiffenend panels. NLL Verslagen en verhandelingen XX1 - 1959. TR F.184. A simplified method for the calculation of three-dimensional laminair boundary layers. NLL Verslagen en verhandelingen XXIII - 1961. TR G.1 Theoretical determination of the power efficiency and overall flow behaviour of free jet wind tunnels with … NLR Verslagen en verhandelingen XXV - 1961. TR S.578. On the analysis of swept wing structures. NLR Verslagen en verhandelingen XXVIII - 1964. TR G.30. On the determination of optium shapes with finite nose angles. NLR Verslagen en verhandelingen XXVIII - 1964. TR S.597. Results of strain measurements performed on a polystyrene sweptback box beam with a non-swept centre part … 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 XXXI - 1965. TR M.2138. The effect of temperature and frequency on the fatigue crack propagation in 2024-T3 Alclad sheet material. 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 69007U. Symmetrical transonic potential flows around quasi-elliptical aerofoil sections. Flight test schedule; after inspection 5 or 6 (Report VD-27-102); F.27 all versions d.d.1-6-1971 (niet ingevuld) Aircraft weighing record; serial no. 10622; registration M-2 d.d. 30-10-1996
