College of Aeronautics: Recent submissions

Now showing items 421-440 of 712

Spontaneous -ignition data of hydrocarbons and aviation fluids

Goodger, E. M. (College of Aeronautics, )
The stability of honeycomb sandwich panels in shear

Nichols, R. (College of Aeronautics, )
The effect of jet deflection on the interference of a rearward facing jet

Craven, A. H. (College of Aeronautics, )
The influence of frame pitch and stiffness on the stress distribution in pressurised cylinders

Houghton, D. S. (College of Aeronautics, )
The design of a multi-cell box in pure bending for minimum weight

Houghton, D.S.; Chan, A. S. L. (College of Aeronautics, )
Vortex tube performance data sheets

Westley, R. (College of Aeronautics, )
Notes on the problem of the optimum design of structures

Hemp, W. S. (College of Aeronautics, )
A transistorized radiation monitor

Brown, D. C.; Faraday, B. P. (College of Aeronautics, )
A note on the discontinuity stresses at the junction of a pressurised spherical shell and a cylinder

Houghton, D. S.; Chan, A. S. L. (College of Aeronautics, )
Optimum design of a multicell box subjected to a given bending moment and temperature distribution

Johns, D. J. (College of Aeronautics, )
Property requirements for liquid rocket propellants

Goodger, E. M. (College of Aeronautics, )
A variable delay line

Brown, D. C. (College of Aeronautics, )
Clearance fits and the limits on mating parts

Harris, J. T. (College of Aeronautics, )
American teaching and practice of industrial engineering and management

Cherry, J. (College of Aeronautics, )
A review of plastics for use in the aircraft industry

Fahy, F. (College of Aeronautics, )
The effect of transition wires on the pressure distribution over a NACA 63A215 aerofoil section

Harris, K. D. (College of Aeronautics, )
The man-propelled aircraft: a preliminary assessment

Nonweiler, T. (College of Aeronautics, )
Method study of hot working conditions

Williams, J. A. C. (College of Aeronautics, )
A preliminary report on the aerodynamic characteristics of a 40 degrees swept back wing of aspect ratio 4.5

Barna, P. S. (College of Aeronautics, )
Stability of a rotating cylindrical shell partially filled with liquid

Ward, G. N. (College of Aeronautics, )

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College of Aeronautics: Recent submissions

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