CoA. Notes (1952-1969): Recent submissions

Now showing items 121-137 of 137

The lift induced on a circular cylinder by a narrow jet emerging at an angle to the uniform stream

Anderson, R. G. (College of Aeronautics, )
Avoidable delays among women workers on light work

Williams, J. A. C. (College of Aeronautics, )
Solution of a load diffusion problem by relaxation methods

Vaisey, Gillian; Hemp, W. S. (College of Aeronautics, )
A resume of maximum lift data for symmetrical wings, with various high-lift aids

Nonweiler, T. (College of Aeronautics, )
Rational presentation of histogram data on samples

Williams, J. A. C. (College of Aeronautics, )
Some bearing materials under high pressures at low rotational speeds

Preston, C. (College of Aeronautics, )
Longitudinal stability characteristics and damping in pitch of delta wings

McCarter, W. B. (College of Aeronautics, )
A preliminary report on the use of the wide angle diffuser in ground mufflers of the type used for silencing jet aircraft

Green, D. J. (College of Aeronautics, )
Investigation of eye movements of an aircraft pilot under blind approach conditions

Watts, A. F. A. (College of Aeronautics, )
A bibliography and survey of the vortex tube

Westley, R. (College of Aeronautics, )
Some notes on the factors influencing the possible damage to buildings due to the passage of shock waves from aircraft flying at supersonic speeds

Lilley, G. M. (College of Aeronautics, )
Factors affecting punching speeds of hollerith operators. Mechanical factors outside the control of the operators

Majewski, T. R. (College of Aeronautics, )
The characteristics of the flow field over the mid-upper fuselage of Lancaster P. A. 474

Burrows, F. M. (College of Aeronautics, )
Trends in aircraft design

Newell, A. F.; Howe, D. (College of Aeronautics, )
Machinability investigations into special materials. Part 1 stainless steel Rex 448 hardened and tempered to Brinell minimum 321, maximum 375

Purcell, J. (College of Aeronautics, )
The calculation of the wave drag of a family of low-drag axisymmetric nose shapes of fineness ratio 4.5 at zero incidence at supersonic speeds

Marson, G. B. (College of Aeronautics, )
The wave drag of highly-swept wings: a comparison of linear theory and slender body theory

Nonweiler, T. (College of Aeronautics, )

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CoA. Notes (1952-1969): Recent submissions

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