Delta 31-483 User Manual download pdf (Page 4)

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22. No. Council No. Tit13 Author(s)

1059 30 107

Tests at

1.82

on an engin?

Griffiths, R. T.

installation with bounda&lQer

diverters for a slender gothia

eniz.

kpt, 1967)

1060

31 270

The infleuence of elevetor movement, Eckford, D. J.

on the normal acoeleration~

experienced by a transport

aircraft in moderate turbulence.

(January, 4969)

1061

30 005

1062

31 065

A technique for studing high Stevens, G. W. H.

velocity drawing in polymers. and

(August, 1966) Eiluett, F. C.

Discreet element analysis of the Dawe, D. J.

lateral vibration of rectangular

lates

in the presence of membrane.

,September, 1968)

1063

20 839

Supersonio lsminar boundary layers Cooke, J. (2.

on cones.

(November,

1966).

1064

29 bo7

Approximate solutions of the Smith, P. D.

three-dimensional lsminar boundary- and

layer momentumintegral equations.

(September, 1967)

Ymw, A. D.

1065

30 345

Flight measurements of wing-tip

vortex motion near the ground.

(January,

1968).

Dee, F. IV.

and

1066

30 406

The stability of boundary conditions Taylor, P. J.

in the numerical solution of the

time-dependent NavierStokes

equations.

(August, 1968).

1067

30 782

Crossflow in turbulent boundary

layers.

(December,

1968).

Cumpsty, N. A.

1068

30 781

A critical examination of the use

Cumpsty, N. A.

of a two-dimensional turbulent

profile family to represent

three-dimensional boundary layers.

(December, 1968).

1069

30 561

Heat transfer in a tube revolving Humphreys, J. F.

1 2 3 4 5 6 7 8 9 10

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