Some studies of pressure distributions on the windward surfaces of conical bodies at high supersonic speeds /

An investigation into a technique for measuring jet interference effects using free-flight models /
by: Greenwood, G. H.
Published: (1967)

Measurements of pressure distribution on a half-model wing-body combination of 55 deg. sweep over a wide range of Reynolds number /
by: Winter, K. G. (Kenneth George), et al.
Published: (1975)

Some mutual interference effects between a 5.7 cone and sonic-leading-edge delta wing at M..-2.49 /
by: Goldsmith, E. L.
Published: (1967)

Measurements of drag, base pressure and base aerodynamic heat transfer appropriate to 8.5 semi-angle sharp cones in free flight at mach numbers from 0.8 to 3.8 /
by: Greenwood, G. H.
Published: (1967)

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

The effect of base bleed on the base pressure of several shrouded and unshrouded propelling nozzles at M [infinity] = 1.96 /
by: Shaw, M. M.
Published: (1967)

Analysis of hinge moment data for rectangular and near rectangular trailing edge controls at supersonic and transonic speeds /
by: Isaacs, Donald
Published: (1966)

Estimation of surface pressures from observed shock-wave envelopes surrounding conical bodies at M = 4.0 /
by: Larcombe, M. J.
Published: (1970)

Some comments on the conditions in a local supersonic flow region /
by: Moulden, Trevor H.
Published: (1968)

The effect of combined boundary-layer suction and base bleed on the drag of a 10 degree cone at M=2.58 /
by: Goldsmith, E. L.
Published: (1970)

Mercury programmes for lifting surface theory calculations on wings oscillating in supersonic flow /
by: Harris, G. Z.
Published: (1966)

The effect at M = 1.7 of removing swept endwalls from a wedge compression intake /
by: Shaw, M. M.
Published: (1968)

The design of compression surfaces for high supersonic speeds using conical flow fields /
by: Jones, John Glynn
Published: (1968)

The calculation of the warp to produce a given load and the pressures due to a given thickness on thin slender wings in supersonic flow /
by: Smith, Jeremy H. B.
Published: (1967)

The pressure distribution at zero lift on a slender delta wing at transonic speeds /
by: Firmin, Michael Charles Peter, 1929-
Published: (1968)

A parametric study of the use of nose blunting to reduce the supersonic wave drag of forebodies /
by: Pugh, P. G., et al.
Published: (1974)

Some exact calculations of the lift and drag produced by a wedge in supersonic flow : either directly or by interference /
by: Roe, P. L.
Published: (1967)

Supersonic flutter derivatives for a series of swept and cropped delta wings /
by: Harris, G. Z.
Published: (1967)

Design of a symmetrical section with specified pressure distribution /
by: Sells, C. C. L. (Christopher Cedric Lytton)
Published: (1969)

A practical approach to the prediction of oscillatory pressure distributions on wings in supercritical flow /
by: Garner, H. C.
Published: (1976)

The calculation of generalised forces on oscillating wings in supersonic flow by lifting surface theory /
by: Harris, G. Z.
Published: (1967)

Forces on cone cylinders at M=3.98 /
by: Moore, K. C.
Published: (1968)

Some results of wind-tunnel tests on an aerofoil section (NPL 9510) combining a 'peaky' upper surface-pressure distribution with rear loading /
by: Hall, D. J. (Aerospace engineer), et al.
Published: (1974)

A free-flight investigation into the effect of body shaping on the zero-lift drag of a wing-body combination at transonic and supersonic speeds /
by: Hamilton, J. A.
Published: (1961)

Measurement of the internal performance of a rectangular air intake having variable geometry compression surfaces at Mach numbers from 1.7 to 2.5.
by: Brown, C. S. (Charles Scorer), et al.
Published: (1973)

Evaluation of a loading form for the calculation of linearised theory pressure distributions on wings with control surfaces having swept hinge lines in steady subsonic flow /
by: Wigley, T. G.
Published: (1976)

The use of surface pitot tubes as skin-friction meters at supersonic speeds /
by: Smith, K. G.
Published: (1964)

Wind-tunnel tests on a rectangular, twin-duct, variable-geometry air intake : at supersonic speeds /
by: Dobson, M. D.
Published: (1967)

The use of air injection to prevent separation of the turbulent boundary layer in supersonic flow /
by: Peake, D. J.
Published: (1967)

A new probe for the direct measurement of stagnation pressure in supersonic flow /
by: Goodyer, M. J.
Published: (1975)

The pressure drag of an aerofoil with six different round leading edges, at transonic and low supersonic speeds /
by: Wilby, P. G.
Published: (1967)

Supersonic Transport.
Published: (1971)

Fan supersonic flutter : prediction and test analysis /
by: Halliwell, D. G.
Published: (1977)

Approximate formulae for the lift and drag of wedge aerofoil sections at high supersonic speeds /
by: Squire, Leonard Charles
Published: (1966)

An experimental investigation of the influence of base bleed on the base drag of various propelling nozzle configurations /
by: Roberts, J. B. (Writer on aerodynamics)
Published: (1967)

Half-body and wing combinations in supersonic flow : a review of some principles and possibilities /
by: Goldsmith, E. L.
Published: (1968)