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Aeronautical Research Council Current Papers: Recent submissions

Now showing items 41-60 of 1393

A comparison of three thick, symmetrical, multi-slot suction aerofoils

N. Gregory; A. R. Curtis (1950)
Preliminary measurements of the aerodynamic damping in pitch of a 12 ft diameter helicopter rotor

C.M. Britland; R.A. Fail (1950)
The effect of propeller thrust on downwash and velocity at tailplane - a collection of data from low speed wind tunnel tests

A. Spence (1950)
Wind tunnel tests on a one-twelfth scale model of a twin-engined military transport. (airspeed C 13/45 ayrshire)

R. Warden (1950)
Hydrodynamic design of seaplane floats

K. M. Tomaszewski (1950)
The heat treatment of flat perspex sheets

E. W. Russell (1950)
Low-speed tunnel investigation of the effect of the body on Cmo and aerodynamic centre of unswept wing-body combinations

A. Anscombe; D. J. Raney (1950)
Determination of the static stability of seaplanes

K.M. Tomaszewski (1950)
The viscid flow of air in a narrow slot

G.L. Shires (1950)
Revised and extended performance characteristics of ram jets

D.F. Collins; Frances M. Gordon (1950)
Transitional friction effects in powered controls with particular reference to hydraulic jacks

F. Holoubek (1950)
The application of jet propulsion to helicopters

Wm. Stewart; M.F. Burle (1950)
The indication of boundary-layer transition on aerofoils in the N.P.L. 20 in. x 8 in. high speed wind tunnel

H.H. Pearcey (1948)

The "liquid film" evaporation method developed by Gray for indicating the position of boundary-layer transition on models in low speed wind tunnels has proved satisfactory in the N.P.L. 20 in. x 8 in. high speed tunnel. ...
Note on sintered metal with a view to its use as a porous surface in distributed suction experiments

J. H. Preston; A. G. Rawcliffe (1950)
Report on measurements of the pressure distribution over a wing of triangular plan form at a Mach number of 2.44

G.H. Lean; K.G. Whitaker (1950)
Note on the interference on a part-wing mounted symmetrically on one wall of a wind-tunnel of octagonal section

H. C. Garner (1950)
Tank tests on the effect of slipstream on the water performance of a large four engined flying boat (Shetland 1)

S. Raymond (1950)
Water stability tests on Saro 37 fitted with shetland hull bottom, wing-tip floats, and tail

I. W. McCaig (1950)
Maximum impact pressures on seaplane hull bottoms

A. G. Smith; I. W. McCaig; W. M. Inverarity (1950)
Tests in the N.P.L. electric tank on a 4:1 axi-symmetrical diffuser having a discontinuity in the wall velocity

F. Cheers; W. G. Raymer (1950)

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