CoA. Reports: Recent submissions

Now showing items 101-120 of 280

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., )
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, )

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