Pressure distributions and flow patterns on some conical shapes with sharp edges and symmetrical cross-sections at M = 4.0 /

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

Measurements of the pitching-moment derivatives on a sharp-edged delta wing in incompressible flow /
by: Woodgate, L.
Published: (1964)

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

A numerical method for calculating the pressure due to thickness on symmetrical wings at zero incidence in supersonic flow /
by: Eldridge, Robert Henry
Published: (1968)

Pressure distributions and flow patterns at M = 4.0 on some delta wings /
by: Squire, Leonard Charles
Published: (1964)

An analysis of the subsonic flow past symmetrical blunt-trailing-edge aerofoil sections at zero incidence, in the absence of a vortex street /
by: Nash, John F.
Published: (1966)

Measurements of pressure distributions and pressure drags at zero incidence on both blunt and sharp axisymmetric forebodies at a mach number of 3 /
by: Ward, L. C.
Published: (1980)

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

Low-speed wind-tunnel experiments on a series of sharp-edged delta wings /
by: Earnshaw, P. B.
Published: (1966)

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)

Further experimental investigation of the characteristics of cambered gothic wings at Mach numbers from 0.4 to 2.0 /
by: Squire, Leonard Charles
Published: (1963)

Pressure distribution on two wings with curved leading edges at supersonic speeds /
by: Narayan, K. Yegna
Published: (1974)

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)

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

A direct iteration method for the calculation of the velocity distribution of bodies of revolution and symmetrical profiles /
by: Vandrey, F.
Published: (1964)

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

Non-linear theory of steady forces on wings with leading-edge flow separation /
by: Garner, Henry Clifford
Published: (1964)

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

A study of the effect of leading-edge modifications on the flow over a 50-deg sweptback wing at transonic speeds /
by: Rogers, E. W. E.
Published: (1962)

Measurements of section pressure distribution at a mach number of 2.0 on a wing of 70 degrees sweep mounted on a waisted body /
by: Winter, K. G.
Published: (1971)

Computation of the velocity field induced by a planar source distribution approximating a symmetrical non-lifting wing in subsonic flow /
by: Ledger, J. A.
Published: (1974)

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)

The bursting of leading-edge vortices : some observations and discussion of the phenomenon /
by: Lambourne, N. C.
Published: (1962)

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)

An equivalence law relating three- and two-dimensional pressure distributions /
by: Lock, R. C.
Published: (1964)

Analysis of the static pressure distribution on a Delta wing in subsonic flow /
by: Kirkpatrick, David L. I.
Published: (1970)

Exploratory investigation of the effects of blowing from the leading edge of a delta wing /
by: Trebble, W. J. G.
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)

An experimental investigation at supersonic speeds of the characteristics of two gothic wings, one plane and one cambered /
by: Squire, Leonard Charles
Published: (1961)

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

Evaluation of pressure distributions on thin wings with distorted control surfaces oscillating harmonically in linearised, compressible, subsonic flow /
by: Marchbank, W. R.
Published: (1976)

An experimental investigation of the structure of a leading-edge vortex /
by: Earnshaw, P. B.
Published: (1962)

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)

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

The effects of ridge excrescences and trailing-edge control gaps on two dimensional aerofoil characteristics /
by: Cook, T. A.
Published: (1972)

Leading-edge buckling due to aerodynamic heating /
by: Mansfield, Eric Harold, 1923-
Published: (1960)