NPL aero report

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Bibliographische Detailangaben
Körperschaften: National Physical Laboratory (VerfasserIn), National Physical Laboratory Aerodynamics Division (Herausgebendes Organ)
Format: UnknownFormat
Veröffentlicht: Teddington, Middlesex 1957-
Schlagworte:
Monografische Reihe
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Titel Jahr Band
Time-average aerodynamic forces on bridges 1971
A comparison between full-scale wind-induced instability of the Wye Bridge and that predicted from sectional-model tests 1970
An investigation of the forces on flat plates in turbulent flow 1969
The oscillations of model circular stacks due to vortex shedding at Reynolds numbers fromm 10 5 to 3.10 6 1968
Simple wind tunnel design 1968
The analogy between streamline curvature and buoyancy in turbulent shear flow 1967
Measurements of the wind forces on a series of models of merchant ships 1967
The application of Maskell's theory of wind-tunnel blockage to very large solid models 1967
The effecct of initial conditions on the development of turbulent boundary layers 1967
The turbulence structure of equilibrium boundary layers 1966
The variation of profile drag with Mach number up to the critical value : a comparison of recent predictions with early flight and wind-tunnel measurements, and a comment on an earlier prediction 1966
A note on the prediction of aerofoil profile drag at subsonic speeds 1966
Calculation of boundary-layer development using the turbulent energy equation 2 Compressible flow on adiabatic walls / by P. Bradshaw and D. H. Ferriss 1966 2
On the flow behind a coarse grid and its use as a model of atmospheric turbulence in studies related to wind loads on buildings : to be presented at the National Physical Laboratory, 7th April 1965, to the Third Meeting on Industrial Aerodynamics Research 1965
The response of a retarded equilibrium turbulent boundary layer to the sudden removal of pressure gradient 1965
The aeroelastic stability of the Severn Suspension Bridge 1964
A note on the howling of ejector shrouds 1963
Wind-tunnel tests on a model forest 1963
Effect of the laminar boundary layer development in a shock tube on spectrum-line reversal temperature measurements 1963
The effect of an initial boundary layer on the development of a turbulent free shear layer 1962
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