The Aeronautical Journal, Volume 73Royal Aeronautical Society, 1969 - Aeronautics |
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Page 795
... Turbine Performance To make a detailed study of the effect of the increased aerodynamic losses due to effusion through a porous tur- bine blade requires a full optimisation of the engine cycle for a given application . Thus , pressure ...
... Turbine Performance To make a detailed study of the effect of the increased aerodynamic losses due to effusion through a porous tur- bine blade requires a full optimisation of the engine cycle for a given application . Thus , pressure ...
Page 925
... turbine entry tempera- ture . Advanced turbine cooling methods do not diminish the need for materials of higher strength and improved cor- rosion resistance . Apart from their primary contribution towards increasing turbine entry ...
... turbine entry tempera- ture . Advanced turbine cooling methods do not diminish the need for materials of higher strength and improved cor- rosion resistance . Apart from their primary contribution towards increasing turbine entry ...
Page 926
... turbine entry temperatures , to main- tain combustion wall temperature at 700 ° C by improve- ment of cooling ... Turbine Turbine Jet ENGINES Jet able contribution towards the solution of these problems , but additionally there is a need ...
... turbine entry temperatures , to main- tain combustion wall temperature at 700 ° C by improve- ment of cooling ... Turbine Turbine Jet ENGINES Jet able contribution towards the solution of these problems , but additionally there is a need ...
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Aero aerodynamic aerofoil Aeronautical Journal aeroplane air transport airline airport angle application associated Aviation blade boundary layer British BRITISH AIRCRAFT CORPORATION cargo CEng civil Civil Air Transport configuration conventional cost cross-coupling dynamic effect engine equipment fibres field Figure flight flow flying FRAeS fuselage future Harrier Hawker Siddeley Aviation helicopter hover Illustrated increase industry lecture lift lift-fan London Mach number man-powered flight mechanical ment methods military NASA TN noise level obtained operation organisation outer space paper passengers performance pilot plate polymers possible present problem programme propulsion ratio rotorcraft Royal Aeronautical Society Royal Air Force satellite shown in Fig speed STOL structure Sud Aviation supersonic tail rotor take-off technical techniques Technology temperature thrust tion traffic turbine V/STOL vector vehicle velocity VTOL weight Westland wing