Wind-tunnel tests on a rectangular, twin-duct, variable-geometry air intake : at supersonic speeds /

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

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

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

Supersonic inlets /
by: Faro, Ione D. V.
Published: (1965)

Measurement of the internal drag of air breathing installations on slender wing-body combinations at supersonic speeds /
by: Britton, J. W.
Published: (1967)

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

Boundary-layer interaction effects in intakes with particular reference to those designed for dual subsonic and supersonic performance /
by: Seddon, J.
Published: (1970)

A supersonic tunnel design for testing engine intakes /
by: Staniforth, R.
Published: (1961)

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets /
by: Trefny, Charles J., et al.
Published: (1986)

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)

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

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

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

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

Air intake problems in supersonic propulsion ; invited papers presented at the 11th AGARD Combustion and Propulsion Panel meeting, Paris, December 1956 /
Published: (1958)

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

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

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)

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)

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)

Tests on an engine installation for a slender gothic wing at M-1.82 /
by: Griffiths, R. T.
Published: (1967)

Low-speed wind-tunnel measurements of damping in yaw (n[psi]) on an A.R. 9 jet-flap complete model /
by: Cox, A. P.
Published: (1967)

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)

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)

Aerodynamic performance of flared fan nozzles used as inlets /
by: Dietrich, Donald A., et al.
Published: (1976)

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

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

Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack /
by: Latham, Eldon A.
Published: (1976)

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

Design and operation of intermittent supersonic wind tunnels /
by: Ferri, Antonio, 1912-
Published: (1954)

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

Further tests with a variable ramp intake having a design Mach number of 2.2 /
by: Neale, M. C.
Published: (1966)

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

High-speed flight propulsion systems /
Published: (1991)

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

Aerodynamic components of aircraft at high speeds /
by: Donovan, A. F. (Allen F.)
Published: (1957)