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DECROIX PAUL
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DECROIX PAUL
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Werkwijze en inrichting voor het aanbrengen van een jaloezie-lamel of een overeenkomstige lamel- lenband bij de vervaardiging van een ophaalbare lamellenjaloezie.
Pressure distributions on a wing having NACA 4415 airfoil sections with trailing-edge flaps set at 0 deg and 40 deg(Wind tunnel measurements of pressure distributions on wing having NACA 4415 airfoil sections with trailing-edge flaps set at 0 deg and 40 deg)
Some characteristics of the hydrodynamics of an engine of the flapping wing type(Characteristics and advantages of flapping wing engine over screw engine)
Investigations of swept wings with supersonic leading edges low drag boundary layer suction experiments on a 36 deg swept wing at mach numbers 2. 5, 3. 0, and 3. 5(Investigation of swept wings with supersonic leading edges- low drag boundary layer suction experiments on 36 degree swept wings at Mach numbers 2. 5, 3. 0, and 3. 5)
Comparison of the treatment of the thickness problem of a delta wing with sonic leading edges and the theory of transonic flow(Method of characteristics used in solving nonlinear boundary value problem of thickness of delta wing with transonic leading edge)
Variation of a meteor spectrum during the time of flight(Meteor spectrograms used to determine intensity distributions at various points of trajectory)
Investigation of the flow in the vicinity of V-shaped wings formed by the boundaries of the flow behind a plane shock wave(V-shaped wings with plane sides and sharp edges investigated for aerodynamic properties, deriving equations for flow parameters at Mach 6)
Preliminary measurements of the flow field on the leeside of a delta wing of unit aspect ratio at a mach number of 2. 6 and an incidence of 15 dec(Flow field on leeside of delta wing of unit aspect ratio- wind tunnel tests at Mach 2. 6 and incidence angle 15 deg)
Effect of wing tip shape on vortex sheet rolling up(Effect of wing tip shape on vortex sheet rolling up applied to study of straight or moderately sweptback wings)