Incompressible flow over delta wings /

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

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

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

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)

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)

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

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

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

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

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

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

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)

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)

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

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

Experimental investigation of the positions of the leading-edge vortices above slender delta wings with various rhombic cross-sections in subsonic conical flow /
by: Kirkpatrick, David L. I.
Published: (1967)

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

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 of the effects of thickness on vortex breakdown position on a series of sharp-edged delta wings /
by: Earnshaw, P. B.
Published: (1968)

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)

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

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

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)

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 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)

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

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

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)

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)

Aileron control of small-aspect-ratio aircraft ; in particular, Delta aircraft /
by: Pinsker, W. J. G.
Published: (1960)

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)

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

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)

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)