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Showing 10 out of a total of 1003 results for community: Aeronautical Research Council. (0.187 seconds)

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An investigation at transonic speeds of the performance of various distributed rougness bands used to cause boundary-layer transition near the leading edge of a cropped delta half-wing

E.W.E. Rogers et al (1960)
On the driver-reservoir technique Part 1 Application to shock and gun tunnels Part 2 Determination of optimum reservoir size

L. Davies; K. Dolman; D. R. Brown; G. Hooper (1968)
Notes on some experimental and theoretical results for the boundary layer development aft of the shock in a shock-tube

L. Bernstein (1963)
Static tests of ground effect on planforms fitted with a centrally-located round lifting jet

L. A. Wyatt (1964)
Fatigue loadings in flight - loads in the tailplane of a devon

Anne Burns (1960)
A short static probe with good incidence characteristics at supersonic speed

I. S. Donaldson; D. J. Richardson (1967)
The cooling performance of two extruded-type air-cooled turbine nozzle blades

R. I. Hodge (1960)
Crack propagation properties of thin sheet - some recent results and their impact on design

Williams, D. (1961)
Experiments at hypersonic speeds on circular cones at incidence

D.H. Peckham (1965)
The performance of a conical convergent-divergent nozzle with area ratio 2.9 in external flow

G. T. Golesworthy; M. V. Herbert (1966)

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