Further tests with a variable ramp intake having a design Mach number of 2.2 /

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

A simple flexible supersonic wind tunnell nozzle for the rapid and accurate variation of flow mach number /
by: Pierce, D.
Published: (1967)

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

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

Measurement of the internal performance of a rectangular air-intake at Mach number of 0.9 /
by: Brown, C. S. (Aerospace engineer), et al.
Published: (1976)

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

Characteristics of aft-mounted all-moving rectangular control surfaces on a slender cruciform model at mach numbers from 0.6 to 2.8 /
by: Winter, Kenneth George
Published: (1968)

The performance of conical convergent-divergent nozzles of area ratios 2.44 and 2.14 in external flow /
by: Golesworthy, G. T.
Published: (1967)

The performance of a conical convergent-divergent nozzle with area ratio 2.9 in external flow /
by: Golesworthy, G. T.
Published: (1967)

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

Tests at a mach number of 2.0 on a rectangular twin-duct air intake with variable geometry : situated in the flow field of a slender wing /
by: Dobson, M. D.
Published: (1970)

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

Characteristics of high-speed wind tunnels in the United Kingdom relevant to aeroelastic-model tests /
by: Irwin, C. A. K.
Published: (1967)

The performance of a centrebody propelling nozzle with a parallel shroud in external flow.
Published: (1966)

The performance of a centrebody propelling nozzle with a parallel shroud in external flow.
by: Herbert, M. V., et al.
Published: (1966)

The effect of external flow on an internal-expansion propelling nozzle incorporating ventilation by ambient air /
by: Herbert, M. V.
Published: (1966)

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

A technique for the wind tunnel simulation of store release at high speeds /
by: Beecham, L. J.
Published: (1966)

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)

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 correlation and prediction of pressure distributions on compression surfaces of sharp-edged conical bodies at high supersonic speeds /
by: Larcombe, M. J.
Published: (1969)

Boundary layer separation in a centrebody nozzle with parallel shroud /
by: Herbert, M. V., et al.
Published: (1966)

A prediction method for pressure distributions on compression surfaces of conical bodies at supersonic speeds /
by: Larcombe, M. J.
Published: (1974)

Further results on the mixing of free axially-symmetrical jets of mach number 1.40 /
by: Johannesen, N. H.
Published: (1962)

Simple theoretical and experimental studies of the flow through a three-shock system in a corner /
by: Eminton, E.
Published: (1966)

Supersonic laminar boundary layers on cones /
by: Cooke, J. C. (John Caister)
Published: (1969)

The economic effects of meteorological forecasting standards for supersonic civil transports /
by: Courtney, Adrian Laurence
Published: (1969)

Some studies of pressure distributions on the windward surfaces of conical bodies at high supersonic speeds /
by: Akers, Arthur
Published: (1966)

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

Measurement of the internal performance of a rectangular air intake mounted on a fuselage at mach numbers from 1.6 to 2.
by: Brown, C. S. (Aerospace engineer), et al.
Published: (1974)

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

Leading edge effects on caret wings /
by: Cooke, J. C. (John Caister)
Published: (1968)

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)

Vertical accelerations due to structural vibrations of a slender aircraft flying in continuous turbulence /
by: Zbrozek, J. K.
Published: (1966)

Interim report on low-speed flight tests of a slender-wing research aircraft (Handley Page H. P. 115) /
by: Bisgood, P. L.
Published: (1966)