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ONCE again we are enabled, through the courtesy of the Institution of Mechanical Engineers, to publish a paper which is of outstanding importance in the development of internal combustion turbine engines.
THE twentieth Salon International de l'Aronautique was held from June 26 to July 5, the stands being housed in a new permanent building at the southeastern extremity of the airport of le Bourget with the outside static aircraft part and runways nearby. Apart from being much more convenient for...
To facilitate future development of the cooled gasturbine, more test information is needed on the effectiveness of cooling in an actual turbine operating at high gastemperatures. Part I of this paper deals with some design aspects of a singlestage experimental turbine built to enable an...
IF the plane of symmetry of the wheel is the same in both its landing and retracted positions, retraction is achieved by simple rotation about an axis which is perpendicular to the plane of the wheel.
THERE are various approaches to the problem of the evolution of a line of production aircraft from the basic prototype machine and the merits and demerits of each will depend to some extent on the kind of aircraft, the local conditions and the magnitude of the production order.
Under this heading are published regularly abstracts of all Reports and Memoranda of the Aeronautical Research Council, Reports and Technical Memoranda of the United States National Advisory Committee for Aeronautics and publications of other similar Research Bodies as issued
A method for detachably fitting the end connexions of highpressure flexible hose assemblies has been developed by Bowden Engineers Ltd., Willesden Junction, London, N.W.10. The arrangement, as shown in fig 1, provides that the fitting grips firmly the wirebraid reinforcement.
To maintain liquidtightness in an integral wing fuel tank at the junction of the stringers 12, 13 and the bulkhead 10 forming the end wall of the tank, each stringer is divided into inner and outer portions 12, 13 respectively, the webs of the two portions being in alignment and bolted to a...
Jet propelled apparatus comprising a combustion chamber, a casing surrounding the side wall of said chamber and enclosing a jacket space, means to supply liquid fuel to said jacket space, an annular collecting member at the rear end of said side wall to which said liquid fuel is delivered from...
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