College of Aeronautics: Recent submissions

Now showing items 121-140 of 712

Notes on research into some aspects of stall-warning devices

Bethwaite, C. F.; Langley, R. A. (College of Aeronautics, Cranfield, )
The instrumentation of an aircraft (De Havilland "dove") for flight-test instruction

Bethwaite, C. F.; Newell, A. F. (College of Aeronautics, Cranfield, )
Some experiments on the flow in the boundary layer of a 45 degrees sweptback untapered wing of aspect ratio 4

Emslie, K.; Hosking, L.; Marshall, W. S. D. (College of Aeronautics, Cranfield, )
The numerical solution of certain differential equations occurring in Crocco's theory of the laminar boundary layer

Kirkby, S.; Nonweiler, T. (College of Aeronautics, Cranfield, )
Surface conduction of the heat transferred from a boundary layer

Nonweiler, T. (College of Aeronautics, Cranfield, )
The distribution of pressure over the surface of wings of small aspect ratio

Marshall, W. S. D. (College of Aeronautics, Cranfield, )
An investigation of the flexure-torsion flutter characteristics of aerofoils in cascade.

Lilley, G. M. (College of Aeronautics, Cranfield, )
The laminar boundary layer in slip flow

Nonweiler, T. (College of Aeronuatics, Cranfield, )
Optimum climb technique for a jet propelled aircraft

Kelly, L (College of Aeronautics, Cranfield, )
The strain energy analysis of swept boxes with ribs normal to the spars

Howe, D. (College of Aeronautics, Cranfield, )
Dynamic aeroelasticity of aircraft with swept wings

Radok, J. R. M. (College of Aeronautics, Cranfield, )
The theory of general instability of cylindrical shells

Radok, J. R. M. (College of Aeronautics, Cranfield, )
Analysis of experiments on swept wing structures

Howe, D. (College of Aeronautics, Cranfield, )
Analysis of two-cell swept box with ribs parallel to the line of flight under loading by constant couples

Howe, D. (College of Aeronautics, Cranfield, )
The two-dimensional laminar boundary layer at hypersonic speeds

Nonweiler, T. (College of Aeronautics, Cranfield, )
The potential due to a source moving through a compressible fluid and applications to some rotary derivatives of an aerofoil

Westley, R. (College of Aeronautics, Cranfield., )
Theoretical stability derivatives of a highly swept delta wing and slender body combination

Nonweiler, T. (College of Aeronautics, Cranfield, )
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, )

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College of Aeronautics: Recent submissions

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