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Now showing items 141-160 of 3498

The determination in flight of the body drag and the mean blade profile drag coefficient of a helicopter

Bartholomew, F. E.; Marshall, W. S. D. (College of Aeronautics, Cranfield, )
Stress distribution near a rectangular cut-out in a reinforced circular cylinder due to direct shear loading and torque. part 1, test results

Henson, G. S. (College of Aeronautics, Cranfield, )
Aileron reversal and divergence of swept wings with special consideration of the relevant aerodynamic and elastic characteristics

Radok, J. R. M. (College of Aeronautics, Cranfield, )
The profile drag of yawed wings of infinite span

Young, A. D.; Booth, T. B. (College of Aeronautics, Cranfield., )
Wave reflection near a wall

Robinson, A. (College of Aeronautics, Cranfield., )
Flutter and divergence of sweptback and sweptforward wings

Babister, A. W. (College of Aeronautics, Cranfield., )
Nose controls on delta wings at supersonic speeds

Bolton Shaw, B. W. (College of Aeronautics, Cranfield., )
The use of a potential flow tank for testing axi-symmetric contraction shapes suitable for wind tunnels

Babister, A. W.; Marshall, W. S. D.; Lilley, G. M.; Sills, E. C.; Deards, S. R. (College of Aeronautics, Cranfield., )
Measurements of the pressure distribution on swept back wings with trailing edge split flaps: summary of wind tunnel work at the College of Aeronautics 1948 - 50

Babister, A. W. (College of Aeronautics, Cranfield., )
The equations of motion and energy and the velocity profile of a turbulent boundary layer in a compressible fluid

Young, A. D. (College of Aeronautics, Cranfield., )
Tests on the general instability of a stiffened metal cylinder under axial compression

Heald, W. R. (College of Aeronautics, Cranfield., )
Aerofoil theory for swallow tail wings of small aspect ratio

Robinson, A. (College of Aeronautics, Cranfield., )
The evaluation of matrix elements for the analysis of swept-back wing structures by the method of oblique coordinates

Lewis, S. R. (College of Aeronautics, Cranfield., )
Stability of the compressible laminar boundary layer with an external pressure gradient

Laurmann, J. A. (College of Aeronautics, Cranfield, )
Note on the efficiency of adiabatic shock

Morley, A. W. (College of Aeronautics, Cranfield., )
Vibrations of a swept box

Radok, J. R. M. (College of Aeronautics, Cranfield, )
An investigation of boundary layer effects on two dimensional supersonic aerofoils

Zienkiewicz, H. K. (College of Aeronautics, Cranfield, )
The aerodynamic derivatives with respect to rate of yaw for a delta wing with small dihedral at supersonic speeds

Hunter-Tod, J. H. (College of Aeronautics, Cranfield, )
Experiments on an induction type high speed wind tunnel driven by low pressure steam

Lilley, G. M.; Holder, D. W. (College of Aeronautics, Cranfield, )
The buckling in compression of panels with square top-hat section stringers

Hemp, W. S.; Griffin, K. H. (College of Aeronautics, Cranfield, )

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