Low-speed wind-tunnel tests on a series of uncambered slender pointed wings with sharp edges /

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

Design of warped slender wings with the attachment line along the leading edge /
by: Weber, J.
Published: (1965)

Non-conical flow past slender wings with leading edge vortex sheets /
by: Clark, R. W.
Published: (1978)

Pressure-plotting and force tests at Mach numbers up to 2.8 on an uncambered slender wing of p = 1/2, s/co = 1/4 ('Handley Page Ogee') /
by: Courtney, Adrian Laurence
Published: (1964)

Oscillatory pressure measurements on a flexible slender-wing model at low subsonic speeds /
by: Ruddlesden, F.
Published: (1969)

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

Low-speed wind-tunnel tests on a sweptback wing model (Buccaneer Mark I) with blowing at the wing leading edge and blowing over the flaps and drooped ailerons /
by: Butler, S. F. J.
Published: (1971)

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

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

Low-speed wind-tunnel tests of the longitudinal stability characteristics of some swept-wing quiet airbus configurations /
by: Kirby, D. A. (Donald Allen), 1926-
Published: (1977)

A comparison of results in the A.R.A. transonic tunnel on a small and a large model of a slender wing /
by: Bateman, T. E. B.
Published: (1962)

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)

Pressure distribution on two wings with curved leading edges at supersonic speeds /
by: Narayan, K. Yegna
Published: (1974)

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)

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

The subcritical response and flutter of a slender wing model aircraft /
by: Payen, D. B.
Published: (1969)

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

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

The calculation of lateral stability derivatives of slender wings at incidence, including fin effectiveness, and correlation with experiment /
by: Ross, A. Jean
Published: (1965)

Dynamic tests on free-flying models of slender wings subjected to sidegusts /
by: Gray, William Edrington
Published: (1968)

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)

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

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

The characteristics of some slender cambered gothic wings at Mach numbers from 0.4 to 2.0 /
by: Squire, Leonard Charles
Published: (1964)

Wall corrections for wings oscillating in wind tunnels of closed rectangular section /
by: Acum, Wilfred Ethelbert Aldred
Published: (1963)

Subsonic wind-tunnel tests on a crescent-winged aircraft, including tests of leading-edge droop designs and several tailplane heights /
by: Hall, C. N.
Published: (1961)

A lifting surface theory method for treating swept or slender wings in attached subsonic flow /
by: Kellaway, W.
Published: (1975)

The interference on a three-dimensional jet-flap wing in a closed wind tunnel /
by: Maskell, E. C.
Published: (1961)

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

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)

Upwash interference on wings of finite span in a rectangular wind tunnel with closed side walls and porous-slotted floor and roof /
by: Holder, D. R.
Published: (1965)

Wind-tunnel experiments on a rectangular-wing jet-flap model of aspect-ratio 6 /
by: Alexander, A. J.
Published: (1964)

Rolling-power tests on an elastic model wing (M-planform) in low-speed flow /
by: Gaukroger, D. R. (Donald Richard)
Published: (1964)

Wind tunnel studies of leading edge separation phenomena on a quarter scale model of the outer panel of the Handley Page 'Victor' wing : with and without nose droop /
by: Wallis, R. Allan
Published: (1967)