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Showing 10 out of a total of 79 results for community: Aeronautical Research Council. (0.165 seconds)

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Mechanical Aspects of Turbine Blade Cooling Part I. Description of an Experimental High-Temperature Turbine and Associated Test Rig (Cooled Turbine No. 126) Part II. The Behaviour of Extruded Air-Cooled Rotor Blades Subjected to Steady High Temperature an

N.E. Waldren; et al (1962)
A review of research on two-dimensional base flow

J. F. Nash (1962)
Tip-clearance flow and losses for an isolated compressor blade

B. Lakshminarayana; J. H. Horlock (1962)
On obtaining solutions to the navier-stokes equations with automatic digital computers

D.B. Russell (1962)
An experiment on aerodynamic nozzles at M = 2

J. Reid (1962)
An analysis of two-dimensional turbulent base flow, including the effect of the approaching boundary layer

J. F. Nash (1962)
Pressure measurements on a cone-cylinder-flare configuration at M = 6.85 and incidences up to 30 degrees

D. H. Peckham (1962)
Problems associated with the use of a false wall as a reflection plane for half model tests in the de Havilland high speed wind tunnel

D. R. Holder; H. C. Farley (1962)
An investigation of two methods of suppressing shock oscillation ahead of conical centre-body intakes

C. F. Griggs (1962)
Proving tests of a wingtip parachute installation on a venom aircraft, with some measurements of directional stability and rudder power

F. W. Dee (1962)

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- 1962 (79)