An experimental investigation of the characteristics of some plane and cambered 65 delta wings at Mach numbers from 0.7 to 2.0 /

Heat-transfer and pressure measurements on the upper surface of a delta wing at incidence at Mach numbers between 2.0 and 3.6 /
by: Edwards, J. B. W.
Published: (1967)

Calculations of the effects of blowing from the leading edges of a cambered delta wing /
by: Barsby, J. E.
Published: (1978)

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

An investigation of the flow about a plane half-wing of cropped-delta planform and 6 per cent symmetrical section at stream Mach numbers between 0.8 and 1.41 /
by: Rogers, E. W. E.
Published: (1962)

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

Properties of a two-paramenter family of thin conically cambered delta wings by slender-body theory /
by: Cooke, J. C. (John Caister)
Published: (1962)

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)

Iterative method for thick cambered wings in subcritical flow /
by: Sells, C. C. L. (Christopher Cedric Lytton)
Published: (1976)

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)

A study of slender, cambered, conical wings by an electrical resistance network /
by: Ward, H. S.
Published: (1964)

Part I: The flow pattern on a tapered swept-back wing at Mach numbers between 0.6 and 1.6. Part II: Experiments with a tapered swept-back wing of Warren 12 planform at Mach numbers between 0.6 and 1.6 /
by: Hall, Ian Murray
Published: (1962)

Wind tunnel tests on cambered wings of mild gothic planform : parts I and II /
by: Butterworth, P. J.
Published: (1978)

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 use of conical camber to produce flow attachment at the leading edge of a delta wing and to minimize life-dependent drag at sonic and supersonic speeds /
by: Smith, Jeremy H. B.
Published: (1963)

Measurements : at Mach numbers up to 2.8, of the longitudinal characteristics of one plane and three cambered slender 'ogee' wings /
by: Taylor, C. R.
Published: (1963)

Free-flight measurements of pressure and heat transfer on a blunt leading-edge caret wing at design and off-design mach numbers (M [infinity] =0.9 to 3.36) /
by: Greenwood, G.H
Published: (1971)

Tests at transonic speeds on wings with wedge sections and sweep varying between 0 and 60 /
by: Rogers, E. W. E.
Published: (1963)

An experimental investigation of the subsonic longitudinal characteristics of five slender-wing models with gothic planforms /
by: Kirkpatrick, D. L. I.
Published: (1973)

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)

Some applications of 'not-so-slender' wing theory to wings with curved leading edges /
by: Squire, Leonard Charles
Published: (1962)

Experiments on a delta wing with jet-assisted lift /
by: Melbourne, W. H.
Published: (1962)

An experimental investigation of the effect of planform shape on the subsonic longitudinal stability characteristics of slender wings /
by: Kirby, D. A. (Donald Allen), 1926-
Published: (1969)

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

Analysis of the zero-lift wave drag measured on delta wings /
by: Weber, J.
Published: (1978)

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

Calculation of the induced velocity field on and off the wing plane for a swept wing with given load distribution /
by: Sells, C. C. L. (Christopher Cedric Lytton)
Published: (1973)

Effects of wing stiffness and inertia changes on the modes and frequencies of a model delta aircraft /
by: Webb, D. R. B.
Published: (1962)

A three component gun tunnel balance designed for testing thin delta wings /
by: Opatowski, T.
Published: (1971)

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)

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

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)

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)

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)

Some exploratory measurements of leading-edge vortex positions on a delta wing oscillating in heave /
by: Maltby, R. L.
Published: (1965)

Delta wings with longitudinal camber at low speed /
by: Nangia, R. K.
Published: (1970)