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

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)

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)

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)

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 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)

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

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

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)

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)

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

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

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)

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)

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

Measurement of the moments of inertia of the Handley Page H. P. 115 aircraft /
by: Fennell, L. J.
Published: (1967)

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

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)

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

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

Low-speed wind-tunnel measurements of the lift, drag and pitching moment on three symmetrical ogee-wing models and on a symmetrical slender wing-body model /
by: Kirby, D. A. (Donald Allen), 1926-
Published: (1966)

Pressure-plotting and force tests at Mach numbers up to 2.8 on an uncambered slender wing of p = 1/2, s/co = 1/4 ('Handley Page Ogee') /
by: Courtney, Adrian Laurence
Published: (1964)

An analogue computer for on-line correction of wind-tunnel force and moment data /
by: Pecover, B. E.
Published: (1967)

Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a Mach number of 2.01 /
by: Foster, Gerald V.
Published: (1959)

A study of efficient means of solving transonic flow problems /
by: Trevino, John, 1959-
Published: (1983)

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

Toward Mach 2 : the Douglas D-558 program /
Published: (1999)