Some unseparated base flows with heat addition /

Conditions for the existence of an inertial subrange in turbulent flow /
by: Bradshaw, P. (Peter), 1935-
Published: (1969)

An investigation of the flow about circular cylinders placed normal to a low-density, supersonic stream /
by: Metcalf, S. C.
Published: (1965)

Leakage and secondary flows in compressor cascades /
by: Lakshminarayana, B.
Published: (1967)

Some observations of the flow over a deltawinged model with 55-deg leading-edge sweep, at Mach numbers between 04 and 18 /
by: Sutton, E. P.
Published: (1960)

A theoretical exploration of the flow about an electric arc transverse to an airstream using potential flow methods /
by: Broadbent, E. G.
Published: (1968)

An experimental investigation of the interaction between a forward-facing step and a laminar boundary layer in supersonic, low-density flow /
by: Rogers, E. W. E.
Published: (1967)

Some notes on the flow patterns observed over various swept-back wings at low Mach numbers : (in the R.A.E. 10-ft x 7-ft high speed tunnel) /
by: Haines, A. B.
Published: (1960)

Pressure distribution and surface flow on 5% and 9% thick wings with curved tip and 60 sweepback /
by: Garner, Henry Clifford
Published: (1962)

The effect of forward speed on the inlet flow distribution and performance of a lifting fan installed in a wing /
by: Gregory, Nigel
Published: (1965)

Tip-clearance flow and losses for an isolated compressor blade /
by: Lakshminarayana, B.
Published: (1963)

An investigation of the flow about a plane half-wing of cropped-delta planform and 6 per cent symmetrical section at stream Mach numbers between 0.8 and 1.41 /
by: Rogers, E. W. E.
Published: (1962)

An analysis of the flow over two 45-deg sweptback wings at high subsonic speeds, and comparison with theory /
by: Cook, R.
Published: (1961)

Flight determination of wing flow patterns and buffet boundaries for the Fairey Delta 2 aircraft at Mach numbers between 0.4 and 1.3 : and comparison with wind tunnel results /
by: Dee, F. W.
Published: (1967)

The development of a nozzle for absolute airflow measurement by pitot-static traverse /
by: Ascough, John Cecil
Published: (1964)

The normal impingement of a circular air jet on a flat surface /
by: Bradshaw, P. (Peter), 1935-
Published: (1961)

Part I: The flow pattern on a tapered swept-back wing at Mach numbers between 0.6 and 1.6. Part II: Experiments with a tapered swept-back wing of Warren 12 planform at Mach numbers between 0.6 and 1.6 /
by: Hall, Ian Murray
Published: (1962)

Further experimental investigation of the characteristics of cambered gothic wings at Mach numbers from 0.4 to 2.0 /
by: Squire, Leonard Charles
Published: (1963)

A method of performance estimation for axial-flow turbines /
by: Ainley, D. G.
Published: (1951)

Determination of skin friction, separation and transition with a thin film-heated element /
by: Bellhouse, B. J.
Published: (1967)

Interference problems on wing-fuselage combinations in inviscid, incompressible flow /
by: Weber, J.
Published: (1976)

The steady laminar incompressible boundary-layer problem as an integral equation in Crocco variables : investigation of the similarity flows /
by: Mills, R. D.
Published: (1968)

The structure and behaviour of laminar separation bubbles /
by: Gaster, Michael
Published: (1969)

Unseparate : modernism, interdisciplinary art, and network aesthetics /
by: Madoff, Steven Henry
Published: (2025)

The laminar boundary layer on an inclined cone /
by: Cooke, J. C. (John Caister)
Published: (1967)

Approximate calculation of three-dimensional laminar boundary layers /
by: Cooke, J. C. (John Caister)
Published: (1961)

Two-dimensional laminar compressible boundary-layer programme for a perfect gas /
by: Sells, C. C. L. (Christopher Cedric Lytton)
Published: (1968)

Some possible effects of transonic speeds on wing-aileron flutter /
by: Broadbent, E. G.
Published: (1962)

The performance of some axisymmetric isentropic centrebody intakes designed for mach numbers of 2.48 and 3.27 /
by: Goldsmith, E. L.
Published: (1969)

The measurement of air flow /
by: Ower, E. (Ernest), 1894-
Published: (1966)

The measurement of air flow.
by: Ower, E. (Ernest), 1894-
Published: (1949)

The measurement of air flow /
by: Ower, E. (Ernest), 1894-
Published: (1977)

The effect of internal contraction, initial rate of subsonic diffusion, and cowl and contrebody shape on the pressure recovery of a conical-centrebody intake at supersonic speeds /
by: Goldsmith, E. L.
Published: (1962)

Possible losses in airspeed during turning manoeuvres in gusty air /
by: Pinsker, W. J. G.
Published: (1971)

Empire of the air ; the advent of the air age, 1922-1929.
by: Templewood, Samuel John Gurney Hoare, Viscount, 1880-1959
Published: (1957)

The measurement of skin friction in supersonic flow by means of heated thin film gauges /
by: Bellhouse, B. J.
Published: (1968)

On the prediction of base pressure on two-dimensional supersonic turbulent flow /
by: Roberts, J. B. (Writer on aerodynamics)
Published: (1966)