The performance of some axisymmetric isentropic centrebody intakes designed for mach numbers of 2.48 and 3.27 /

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

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

Oscillatory aerodynamic forces in linearised supersonic flow for arbitrary frequencies, planforms and mach numbers /
by: Allen, D. J.
Published: (1965)

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)

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)

More tests with a variable ramp intake having a design mach number of 2.2 /
by: Neale, M. C.
Published: (1967)

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

On the static performance of two-dimensional intakes with momentum injection in the form of boundary-layer control by blowing /
by: Gregory, Nigel
Published: (1971)

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

Some tests with a variable ramp intake having sidewall compression and a design mach number of 2.2 /
by: Neale, M. C.
Published: (1967)

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)

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

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

Charts of peak amplitudes in incidence and sideslip in rolling manoeuvres due to inertia cross coupling /
by: Pinsker, W. J. G.
Published: (1962)

The velocity potential on triangular and related wings with subsonic leading edges oscillating harmonically in supersonic flow /
by: Davies, David Eric
Published: (1961)

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

Minimum drag surfaces of given lift which support two-dimensional supersonic flow fields /
by: Pike, Jack, 1937-
Published: (1968)

A form of the supersonic flow equations for an ideal gas /
by: Walkden, F.
Published: (1974)

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

The formulation of an influence-coefficient method for determining static aeroelastic effects : and its application to a slender aircraft in symmetric flight at M = 2.2 /
by: Taylor, A. S.
Published: (1969)

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)

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

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)

Tables of supersonic symmetrical flow around right circular cones : with and without the addition of heat at the wave /
by: Bartlett, Ronald Stanley
Published: (1968)

Experiments with biconvex and double-wedge aerofoils in low-density, supersonic flow /
by: Rogers, E. W. E.
Published: (1970)

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

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

An experimental and theoretical comparison at M=4 of the lift-to-drag ratio of some possible aircraft shapes /
by: Brown, C. S. (Charles Scorer)
Published: (1969)

Theory and tunnel tests of rotor blades for supersonic turbines /
by: Stratford, B. S.
Published: (1962)

Experiments at M b0 s= 4.03 on two families of pressure-plotting wing-and-half-cone combinations /
by: Rogers, E. W. E.
Published: (1967)

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)

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)

Some calculations of the take-off behaviour of a slender-wing supersonic transport design constrained to follow a specified pitch-attitude time history /
by: Tomlinson, Barry Nigel
Published: (1967)

Measurement of the pitching-moment derivatives for rigid tapered wings of hexagonal planform oscillating in supersonic flow /
by: Woodgate, L.
Published: (1962)

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