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Now showing items 101-120 of 3498

The application of memo-motion to industrial operations

Norbury, C. J. (College of Aeronautics, Cranfield., )
An investigation into the machining of titanium 150A in the Forged State

Holt, J. T. D. (College of Aeronautics, Cranfield., )
The flexure-torsion flutter of cambered aerofoils in cascade

Craven, A. H. (College of Aeronautics, Cranfield., )
The combustion characteristics of a cylindrical-rod burner system

Goodger, E. M. (College of Aeronautics, Cranfield., )
The economics of aircraft production : a study of the control of overhead costs in aircraft manufacture

Twiss, B. C. (College of Aeronautics, Cranfield., )
Measurement of the derivative zw for oscillating sweptback wings

Whitmarsh, G. E. (College of Aeronautics, Cranfield., )
An investigation into the effect of the application of sub sonic vibrations during the period of solidification of castings with particular reference to a material for gas turbine blades - 'H.R. Crown Max'

Hinchcliff, S. (College of Aeronautics, Cranfield., )
Note on the results of some profile drag calculations for a particular body of revolution at supersonic speeds

Wedderspoon, J. R. (College of Aeronautics, Cranfield., )
An experimental investigation into some of the problems associated with stress diffusion in the vicinity of chord-wise cut-outs in the wing, and a comparison with existing theories

Brown, L. W. (College of Aeronautics, Cranfield., )
On the synthesis of 3-terminal RC networks

Adams, K. M. (College of Aeronautics, Cranfield, )
On some aspects of the noise propagation from supersonic aircraft

Lilley, G. M.; Westley, R.; Yates, A. H.; Busing, J. R. (College of Aeronautics, Cranfield, )
The theoretical wave drag at zero lift of fully-tapered swept wings of arbitrary section

Nonweiler, T. (College of Aeronautics, Cranfield, )
Testing and analysis of a 60 degrees swept back wing with ribs parallel to the line of flight

Howe, D. (College of Aeronautics, Cranfield, )
The calculation of the profile drag of aerofoils and bodies of revolution at supersonic speeds

Young, A. D. (College of Aeronautics, Cranfield, )
Note on the development of a trailing-edge flap as a stall-detector

Bethwaite, C. F. (College of Aeronautics, Cranfield, )
Estimation of the effects of distortion on longitudinal stability of swept wing aircraft at high speeds (sub-critical mach numbers)

Campion, B. S. (College of Aeronautics, Cranfield, )
Measurement of the derivative zw for oscillating wings in cascade

Milne, R. D. (College of Aeronautics, Cranfield., )
Stress concentration in swept wing panels using photoelastic models

Coiley, G. H. (College of Aeronautics, Cranfield, )
A note on the estimation of some low speed characteristics of delta wings

Rose, R. G. (College of Aeronautics, Cranfield, )
Simulation model of the NFLC Jetstream 31

Cooke, A. K. (College of Aeronautics, Cranfield, )

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