College of Aeronautics: Recent submissions

Now showing items 101-120 of 712

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, )
An experimental investigation of the pressure distributions on five bodies of revolution at Mach numbers of 2.45 and 3.19

Marson, G. B.; Socha, W.; Keates, R. E. (College of Aeronautics, Cranfield, )
The effect of vibrations (sonic and subsonic frequencies) during the period of solidification on the mechanical properties of castings of gas turbine materials with special reference to H. R. Crown Max and Nimonic C. 75

Jagaciak, Jerzy (College of Aeronautics, Cranfield., )
The unsteady aerodynamic forces on deforming, low aspect ratio wings and slender wing-body combinations oscillating harmonically in a compressible flow

Milne, R. D. (College of Aeronautics, Cranfield., )

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College of Aeronautics: Recent submissions

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