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Now showing items 161-180 of 3498

On the natural frequencies of a reinforced circular cylinder

Hemp, W. S. (College of Aeronautics, Cranfield, )
The efficiency of adiabatic expansion

Morley, A. W. (College of Aeronautics, Cranfield, )
Some related oscillation problems

Duncan, W. J. (College of Aeronautics, Cranfield, )
Some notes on the performance of small high speed wind tunnels

Lilley, G. M. (College of Aeronautics, Cranfield, )
The time to achieve peak output with special reference to aircraft production

Stanley, P. J. (College of Aeronautics, Cranfield, )
The characteristics of systems which are nearly in a state of neutral static stability

Duncan, W. J. (College of Aeronautics, Cranfield, )
A comparison of the calculated profile drag coefficients of various low drag wing sections

Dowlen, E. M. (College of Aeronautics, Cranfield, )
On the application of oblique coordinates to problems of plane elasticity and swept-back wing structures

Hemp, W. S. (College of Aeronautics, Cranfield, )
The diffusion of loads in non-rigid circular frames

Lewis, S. R. (College of Aeronautics, Cranfield, )
Technique of the step-by-step integration of ordinary differential equations

Duncan, W. J. (College of Aeronautics, Cranfield, )
Note on the dynamics of a slightly deformable body

Hemp, W. S. (College of Aeronautics, Cranfield, )
The effect of the sweepback of delta wings on the performance of an aircraft at supersonic speeds

Robinson, A.; Davies, F.T. (College of Aeronautics, Cranfield., )
Bound and trailing vortices in the linearised theory of supersonic flow, and the downwash in the wake of a delta wing

Robinson, A.; Hunter-Tod, J. H. (College of Aeronautics, Cranfield, )
On some problems of unsteady supersonic aerofoil theory

Robinson, A. (College of Aeronautics, Cranfield, )
Note on the velocity and temperature distributions attained with suction on a flat plate of infinite extent in compressible flow

Young, A. D. (College Of Aeronautics, Cranfield, )
Source and vortex distributions in the linearised theory of steady supersonic flow

Robinson, A. (College of Aeronautics, Cranfield, )
Application of the linear perturbation theory to compressible flow about bodies of revolution

Young, A. D.; Kirkby, S. (College of Aeronautics, Cranfield, )
The aerodynamic derivatives with respect to sideslip for a delta wing with small dihedral at supersonic speeds

Robinson, A.; Hunter-Tod, J. H. (College of Aeronautics, )
Assessment of errors in approximate solutions of differential equations

Duncan, W. J. (College of Aeronautics, Cranfield, )
The relative accuracy of quadrature formulae of the Cotes' closed type

Kirkby, S. (College of Aeronautics, Cranfield, )

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