Report of the Advisory Committee for the William Froude National Tank for Year ending December 13st, 1925

Analog equipment for processing randomly fluctuating data

Calculation of the flow past slender delta wings with leading edge separation

Lubricant behaviour in concentrated contact. The effect of temperature

Flutter of a two-dimensional, simply supported buckled panel with elastic restraint against edge displacement

Studies of ground effect on a 60º inwardly inclined annular jet. Part II Base plate thrust augmentation and pressure distribution; effects of aspects ration, pressure ratio and height above ground; jet stability

Boundary layer growth in the nozzles of the R.A.E. 8 ft. x 8 ft. supersonic wind tunnel

An experimental method of determining the mean heat transfer coefficient for the nozzle of a solid propellant rocket engine, by means of constant flow calorimetry

The use of surface pilot tubes as skin friction meters at supersonic speeds

Study of heat and mass transfer from non-isothermal surfaces

Laboratory wave generation - A comparison of theoretical and experimental performance

An experimental assessment of the stability of the course line of an I.L.S. localiser ground equipment

An estimate of the effect of underwing nacelles on the aerodynamic efficiency of a supersonic transport aircraft

Force pulse testing of ship models

Methods and charts for estimating skin friction drag in wind tunnel tests with zero heat transfer

Some reactions of perfluoroglutaric acid

Some aspects of the thermal degradation of epoxide resins

An application of Mueller's Monte Carlo method for evaluating the stream function in a two-dimensional, irrotational, incompressible flow in a Bellmouth inlet

Measurements of skin friction on a cambered delta wing at supersonic speeds

The increase in wave drag at supersonic speeds due to surface waviness