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Now showing items 3121-3140 of 3498

Shock speed and running time measurements in the N.P.L. hypersonic shock tunnel

B. D. Henshall (1959)
Atmospheric turbulence encountered by super constellation aircraft

J. R. Heath-Smith (1959)
Some experiments with static tubes at transonic speeds in a slotted-wall wind tunnel

E. W. E. Rogers; I. M. Hall (1959)
Microwave techniques applied to the investigation of ionised gases in shock tubes

D. L. Schultz (1959)
The aerodynamic effects of aspect ratio on control surface flutter

H. Hall; E. W. Chapple (1959)
The Effect of Axial Spacing on the Surge Characteristics of Two Mismatched Axial Compressor Stages

R. C. Turner (1959)
The influence of drag characteristics on the choice of landing approach speeds

D. Lean; R. Eaton (1959)
Preliminary note on the effect of inertia cross-coupling on aircraft response in rolling manoeuvres

W. J. G. Pinsker (1959)
The flow upstream of finite span spoilers at supersonic speeds

A. Stanbrook (1959)
Atmospheric turbulence encountered by bristol freighter aircraft in United Kingdom, West Africa and New Zealand

J. R. Heath-Smith (1959)
An experiment to determine the position of an equivalent actuator disc replacing a blade row of a turbomachine

J. H. Horlock; E. C. Deverson (1959)
The interaction between a weak normal shock wave and a turbulent boundary layer

G. E. Gadd (1959)
Some simple conical camber shapes to produce low lift-dependent drag on a slender delta wing

G. G. Brebner (1959)
Statistical analysis of a particular target manoeuvre

R.W. Bain et al (1959)
A note on the control of secondary flow by using cascades of twisted blades

Moira E. Martin (1959)
A deuce programme for the solution of two-dimensional heat-flow problems

K. I. McKenzie (1958)
The distribution of gusts in the atmosphere an integration of U.K. and U.S. data

N. I. Bullen (1959)
Model tests on an effuser induction scheme for operating a transonic wind tunnel

D. A. Spence; A. S. Bennett (1959)
A simple method of improving the supersonic velocity distribution in a transonic tunnel having slotted walls

C. N. Hall (1959)
An improvement of the velocity distribution predicted by linear theory for wings with straight subsonic leading edges

D. G. Randall (1959)

Now showing items 3121-3140 of 3498

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