The Aeronautical Journal, Volume 73Royal Aeronautical Society, 1969 - Aeronautics |
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Page 793
... flow . This effect will increase consistently with injection rate and is predominant at the higer rates of coolant flow . Secondly , injecting the coolant will tend to destabilise a laminar boundary layer and advance the transition to ...
... flow . This effect will increase consistently with injection rate and is predominant at the higer rates of coolant flow . Secondly , injecting the coolant will tend to destabilise a laminar boundary layer and advance the transition to ...
Page 817
... flow where the net flow is from the trailing edge rather than from the leading edge of the rotor blade section . The small shaded area on the right side of each rotor disc represents regions where net flow over the blade section reaches ...
... flow where the net flow is from the trailing edge rather than from the leading edge of the rotor blade section . The small shaded area on the right side of each rotor disc represents regions where net flow over the blade section reaches ...
Page 998
... flow in the wake of a blunt based body at low speeds is a well known pheno- menon , but drastic changes in the wake structure occur as speeds increase . Somewhere in the transonic ... FLOW IN CORE TRANSITION REGION TURBULENT FLOW IN CORE 998.
... flow in the wake of a blunt based body at low speeds is a well known pheno- menon , but drastic changes in the wake structure occur as speeds increase . Somewhere in the transonic ... FLOW IN CORE TRANSITION REGION TURBULENT FLOW IN CORE 998.
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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