Experimental investigation of the positions of the leading-edge vortices above slender delta wings with various rhombic cross-sections in subsonic conical flow /

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

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

The dynamic stability derivatives of a slender wing : a comparison of theory with free-flight model tests at near-zero lift, M = 0.8 to 2.4 /
by: Turner, K. J.
Published: (1968)

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

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

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

Low-speed wind-tunnel measurements of the lift, drag and pitching moment on three symmetrical ogee-wing models and on a symmetrical slender wing-body model /
by: Kirby, D. A. (Donald Allen), 1926-
Published: (1966)

Supersonic flutter derivatives for a series of swept and cropped delta wings /
by: Harris, G. Z.
Published: (1967)

Tests on an engine installation for a slender gothic wing at M-1.82 /
by: Griffiths, R. T.
Published: (1967)

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

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

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)

The behaviour of a conical vortex sheet on a slender wing near the leading edge /
by: Clapworthy, G. J.
Published: (1977)

Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges /
by: Vigneron, Yvon Clovis
Published: (1978)

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

The Delta wing : history and development /
by: Lippisch, Alexander, 1894-1976
Published: (1981)

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)

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

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

Some early experiments on vortex separation.
by: Fink, Peter Thomas
Published: (1967)

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)

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)

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

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)

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

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)

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)

Exploratory investigation of the effects of blowing from the leading edge of a delta wing /
by: Trebble, W. J. G.
Published: (1968)

Incompressible flow over delta wings /
by: Nathman, James Kirwin
Published: (1976)

An experimental investigation of leading edge vortical flow about a delta wing during wing rock /
by: Nelson, Michael Denis, 1961-
Published: (1991)

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

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)

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