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Showing results 41 to 60 of 5133
Issue DateTitleAuthor(s)
Apr-1951The evaluation of matrix elements for the analysis of swept-back wing structures by the method of oblique coordinatesLewis, S. R.
Sep-1951Stability of the compressible laminar boundary layer with an external pressure gradientLaurmann, J. A.
Nov-1951Theoretical stability derivatives of a highly swept delta wing and slender body combinationNonweiler, T.
Dec-1951An investigation of boundary layer effects on two dimensional supersonic aerofoilsZienkiewicz, H. K.
Jan-1952Stress distribution near a rectangular cut-out in a reinforced circular cylinder due to direct shear loading and torque. part 1, test resultsHenson, G. S.
Jan-1952An investigation of the noise field from a small jet and methods for its reduction.Westley, R.; Lilley, G. M.
Feb-1952The potential due to a source moving through a compressible fluid and applications to some rotary derivatives of an aerofoilWestley, R.
Feb-1952The distribution of pressure over the surface of wings of small aspect ratioMarshall, W. S. D.
Mar-1952Aileron reversal and divergence of swept wings with special consideration of the relevant aerodynamic and elastic characteristicsRadok, J. R. M.
Apr-1952Optimum climb technique for a jet propelled aircraftKelly, L
Apr-1952Dynamic aeroelasticity of aircraft with swept wingsRadok, J. R. M.
Apr-1952The determination in flight of the body drag and the mean blade profile drag coefficient of a helicopterBartholomew, F. E.; Marshall, W. S. D.
May-1952An investigation of the flexure-torsion flutter characteristics of aerofoils in cascade.Lilley, G. M.
May-1952Surface conduction of the heat transferred from a boundary layerNonweiler, T.
Jun-1952The theory of general instability of cylindrical shellsRadok, J. R. M.
Nov-1952The laminar boundary layer in slip flowNonweiler, T.
Jan-1953A note on the estimation of some low speed characteristics of delta wingsRose, R. G.
Jan-1953The two-dimensional laminar boundary layer at hypersonic speedsNonweiler, T.
Feb-1953On some aspects of the noise propagation from supersonic aircraftLilley, G. M.; Westley, R.; Yates, A. H.; Busing, J. R.
Feb-1953Some experiments on the flow in the boundary layer of a 45 degrees sweptback untapered wing of aspect ratio 4Emslie, K.; Hosking, L.; Marshall, W. S. D.
Showing results 41 to 60 of 5133