The effect of combined boundary-layer suction and base bleed on the drag of a 10 degree cone at M=2.58 /

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

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)

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

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)

On the design of wing-body combinations of low zero-lift drag rise at transonic speeds /
by: Lord, W. T.
Published: (1962)

On the numerical evaluation of the drag integral.
by: Eminton, Evelyn
Published: (1963)

Numerical methods for calculating the zero-lift wave drag and the lift-dependent wave drag of slender wings /
by: Weber, J.
Published: (1961)

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)

An analysis of the drag of two annular aerofoils /
by: Young, C.
Published: (1973)

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

Some notes on the zero-lift wave drag of slender wings with unswept trailing edge /
by: Weber, J.
Published: (1961)

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

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)

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)

The variation of profile drag with Mach number up to the critical value : a comparison of recent predictions with early flight and wind-tunnel measurements and a comment on an earlier prediction,cby J. Osborne.
by: Osborne, John
Published: (1968)

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)

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)

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

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

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)

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

Flight measurements of the lift, longitudinal trim and drag of the Fairey Delta 2 at mach numbers up to 1.65 and comparisons with wind-tunnel results /
by: Rose, Robert
Published: (1969)

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

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)

Experiments on two-dimensional base flow at subsonic and transonic speeds /
by: Nash, John F.
Published: (1967)

Use of camber and twist to produce low-drag delta or swept-back wings, without leading-edge singularities, at supersonic speeds /
by: Roper, G. M.
Published: (1961)

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)

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

The use of surface pitot tubes as skin-friction meters at supersonic speeds /
by: Smith, K. G.
Published: (1964)

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)

The calculation of generalised forces on oscillating wings in supersonic flow by lifting surface theory /
by: Harris, G. Z.
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)

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)