Fatigue considerations in view of measured load spectra

An investigation of the static stability and drag of two conical re-entry heads at mach numbers from 0.4 to 1.8

Wind tunnel tests at M=2.0 on interference effects between intake flows in a four-engine nacelle

A model of a rectangular air intake of aspect ratio 8, with all-external compression and a fixed geometry, has been tested at its design Mach number of 2.0 in the 3 ft x 3 ft wind tunnel. The model contained four side-by-side simulated engine cells and tests were made to investigate effects on pressure recovery and mass flow in each of the cells...

Wind tunnel tests at supersonic speeds on a model of the Fairey Delta 2

Results are given of tests at Mach numbers from 1.42 to 2.00, on a 1/24 scale model of the Fairey Delta 2 aircraft. Lift, pitching moment, axial farce, sideforce, yawing moment and rolling moment were measured, giving an assessment of the general stability characteristics, including the effects of airbrakes and a ventral fuel tank. Elevator...

Analyse van de bedrijfsgegevens van het “S.S.Simon Bolivar

Analyse van bedrijfsgegevens van het motorschip Papendrecht

Analyse van de bedrijfsresultaten van het dubbelschroef-motorschip 'Willem Ruys'