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 /

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

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

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

Balance measurements (excluding drag) on a delta wing aircraft at transonic speeds /
by: Shaw, M. M.
Published: (1967)

Measurements of the direct pitching oscillation derivatives for three cropped delta and three arrowhead planforms at subsonic and transonic speeds /
by: Miles, C. J. W.
Published: (1965)

Pressure measurements on a model delta wing undergoing oscillatory deformation /
by: Lambourne, N. C.
Published: (1972)

The lift and drag characteristics of caret wings at Mach numbers between 5 and 10 /
by: Collingbourne, J. R.
Published: (1967)

Wind tunnel tests and theoretical investigations on the effect of a localised mass on the flutter of a delta wind with fixed root /
by: Donno, G. F.
Published: (1962)

An airfoil shape for efficient flight at supercritical Mach numbers /
by: Whitcomb, Richard T.
Published: (1965)

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

Measurements of skin friction on a cambered delta wing at supersonic speeds /
by: Winter, Kenneth George
Published: (1967)

Flow past conically-cambered slender delta wings with leading-edge separation /
by: Barsby, J. E.
Published: (1974)

Calculations of the effect of blowing from the leading edges of a slender delta wing /
by: Barsby, J. E.
Published: (1972)

Accuracy of downwash evaluation by Multhopp's lifting-surface theory /
by: Garner, Henry Clifford
Published: (1966)

Calculations of the steady conical flow past a yawed slender delta wing with leading-edge separation /
by: Pullin, D. I.
Published: (1975)

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)

A momentum analysis of lifting surfaces in inviscid supersonic flow /
by: Roe, P. L.
Published: (1969)

Comparison of three methods for the evaluation of subsonic lifting-surface theory /
by: Garner, Henry Clifford
Published: (1969)

Heat transfer and transition measurements at M=8.5 on a delta model and a flat plate at incidence /
Published: (1969)

Wind-tunnel tests on the effects of an added mass on the flutter of a model delta wing /
by: Hall, Handel
Published: (1962)

Algol 60 programme for Multhopp's low-frequency subsonic lifting-surface theory /
by: Garner, Henry Clifford
Published: (1968)

Gun tunnel measurements of lift : drag and pitching moment on a 20 p0 scone, a flat delta and caret delta wing at a mach number of 8.3 /
by: Opatowski, T.
Published: (1967)

Theory of lifting surfaces oscillating at general frequencies in a subsonic stream /
by: Acum, Wilfred Ethelbert Aldred
Published: (1969)

The separated flows on slender wings in unsteady motion /
by: Lowson, M. V.
Published: (1967)

Flight measurements of the elevator and aileron hinge-moment derivatives of the Fairey Delta 2 aircraft up to a Mach number of 1.6 and comparisons with wind-tunnel results /
by: Rose, Robert
Published: (1967)

The lift and stalling characteristics of a 35 deg. swept back wing designed to have identical chordwise pressure distributions at all spanwise stations when near maximum lift /
by: Woodward, D. S.
Published: (1973)

The pressure distribution at zero lift on a slender delta wing at transonic speeds /
by: Firmin, Michael Charles Peter, 1929-
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)

Experimental investigation of the effect of trailing-edge sweepback on the subsonic longitudinal characteristics of slender wings, by D. L. I. Kirkpatrick and A. G. Hepworth.
by: Kirkpatrick, David L. I.
Published: (1970)

The unsteady forces on finite wings in transient motion /
by: Dore, Barrie Dennis
Published: (1967)

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)

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

Experimental and theoretical study of longitudinal aerodynamic characteristics of delta and double-delta wings at Mach numbers of 1.60, 1.90, and 2.16 /
by: Wood, Richard M., et al.
Published: (1985)

Tests at subsonic and supersonic speeds on a slender cambered wing with fin, underwing engine nacelles and trailing-edge controls /
by: Isaacs, Donald
Published: (1969)

Flight determination of wing flow patterns and buffet boundaries for the Fairey Delta 2 aircraft at Mach numbers between 0.4 and 1.3 : and comparison with wind tunnel results /
by: Dee, F. W.
Published: (1967)

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)