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Showing 10 out of a total of 105 results for community: Aeronautical Research Council. (0.25 seconds)

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Boundary-layer separation in supersonic propelling nozzles

M. V. Herbert; R. J. Herd (1964)
Experiments with cones in low-density flows at mach numbers near 2

E. W. E. Rogers; C. J. Berry; B. M. Davis (1964)
Temperature and pressure studies in the reservoir of a reflected-shock hypersonic tunnel

K. C. Lapworth; J. E. G. Townsend (1964)
Lift due to interference between an aerofoil and an external non-lifting body

S. Neumark (1964)
Experiments concerning the effect of trailing-edge thickness on blade loss and turbine stage efficiency

I. H. Johnston; D. C. Dransfield; D. J. Fullbrook (1964)
The N.P.L. 59 in. x 9 in. boundary-layer tunnel

P. Bradshaw; G. E. Hellens (1964)
Design of a supersonic nozzle

A. McCabe (1964)
Generalised aerodynamic forces on a T-tail oscillating harmonically in subsonic flow

D. E. Davies (1964)
The Unsteady Forces on Finite Wings in Transient Motion. Part I. Initial Aerodynamic Forces Following a Sudden Change of Incidence. Part II. Transient Lift and Moment Functions for Rectangular and Delta Wings

B. D. Dore (1964)
Forces on aerofoils with both incidence and forward speed varying

D. G. Randall (1964)

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- 1964 (105)