Calculations of the effect of blowing from the leading edges of a slender delta wing /

Calculations of the flow over thick, conical, slender wings with leading-edge separation /
by: Smith, J. H. B.
Published: (1972)

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

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)

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

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

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)

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

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

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

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)

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

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

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

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

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)

Low-speed wind-tunnel measurements of the lift, drag, and pitching moment of a series of cropped delta wings /
by: Kirby, D. A. (Donald Allen), 1926-
Published: (1974)

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)

Low-speed wind-tunnel measurements on a thin sharp-edged delta wing with 70 leading-edge sweep : with particular reference to the position of leading-edge-vortex breakdown /
by: Lawford, J. A.
Published: (1963)

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

Investigation of the normal force characteristics of slender delta wings with various rhombic cross-sections in subsonic conical flow /
by: Kirkpatrick, David L. I.
Published: (1967)

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

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

The pressure distribution at zero lift on a slender delta wing at transonic speeds /
by: Firmin, Michael Charles Peter, 1929-
Published: (1968)

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

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)

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

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)

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)

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)

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)

Low-speed wind-tunnel tests on a delta-wing aircraft model (S.R. 177) with blowing over the trailing-edge flaps and ailerons /
by: Butler, S. F. J.
Published: (1966)

A theoretical investigation for delta wings with leading-edge separation at low speeds /
by: Nangia, R. K.
Published: (1970)

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)

The airforces on the low-aspect-ratio rectangular wing oscillating in sonic flow /
by: Davies, David Eric
Published: (1963)