NLR rapport S.647 d.d. 29-4-1966. Aanvullende rekmetingen aan beslaglippen op de hulpliggers van twee F-84F vliegtuigen. NLL rapport Technische Mededeling V.1300 d.d. mei 1947. Berekening en correctie van de aanlooplengte van schroefvliegtuigen. Deel 1: De formule voor de aanlooplengte en de … TD-278 NLR rapport V.1967 d.d. 20-10-1967. Note on the effect of maneuvering flaps on the turn performance of Northrop Norair NF-5 aircraft. 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. A.1205. The field of flow through a helicopter rotor obtained from windtunnel smoke tests. NLL Verslagen en verhandelingen XVIII - 1953. A.1263. Experiments on the two-dimensional flow over a NACA 0018 profile at high angles of attack. 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. F.122. Application of experimental aerodynamic coefficients to flutter calculation. NLL Verslagen en verhandelingen XVIII - 1953. F.129. An approach to lifting surface theory. NLL Verslagen en verhandelingen XVIII - 1953. M.1857. A comparative investigation on the fatigue strength at fluctuating tension of several types of rivited lap joints, … NLL Verslagen en verhandelingen XVIII - 1953. S. 416. Comparative fatigue tests with 24 ST Alclad rivited and bonded stiffenend panels.
