The correlation and prediction of pressure distributions on compression surfaces of sharp-edged conical bodies at high supersonic speeds /

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

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

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

Results and analysis of pressure measurements on two isolated slender wings and slender wing-body combinations at supersonic speeds /
by: Fellows, K. A.
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)

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)

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)

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

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)

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

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

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

The isobars in boundary layers at supersonic speeds /
by: Myring, D. F.
Published: (1967)

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

Effects of suction on the interaction between shock wave and boundary layer at a compression corner /
by: Tanner, L. H.
Published: (1970)

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

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

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

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)

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)

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

Tests with a two-dimensional intake having all-external compression and a design mach number of 2.2 [as printed, as printed]. /
by: Neale, M. C.
Published: (1967)

A shock capturing method for calculating supersonic flow fields /
by: Walkden, F., et al.
Published: (1974)

Experimental verification of predicted static hole size effects on a model with large streamwise pressure gradients /
by: Pugh, P. G.
Published: (1971)

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)

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

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)

The pressure-drag due to blunt leading edges on two-dimensional aerofoils : at transonic and low supersonic speeds /
by: Graham, William James
Published: (1967)

Boundary layer bleed drag at supersonic speeds /
by: Goldsmith, E. L.
Published: (1968)

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

Supersonic Transport.
Published: (1971)

The longitudinal characteristics of three slender 'mild ogee' wings at mach numbers from 0.4 to 2.0 /
by: Mabey, Dennis G.
Published: (1968)

Supersonic aerodynamics : a theoretical introduction.
by: Miles, Edward Roy Cecil, 1896-
Published: (1950)

Supersonic aerodynamics : a theoretical introduction /
by: Miles, Edward Roy Cecil, 1896-
Published: (1961)

The inviscid stability of supersonic flow past a sharp cone /
by: Duck, Peter W.
Published: (1990)