Low-speed wind-tunnel tests on the characteristics of leading-edge air intakes in swept wings /

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)

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)

The subcritical response and flutter of a swept-wing model /
by: Irwin, C. A. K.
Published: (1968)

An investigation of scale effects on the transonic flow over swept wings.
Published: (1980)

Some notes on the flow patterns observed over various swept-back wings at low Mach numbers : (in the R.A.E. 10-ft x 7-ft high speed tunnel) /
by: Haines, A. B.
Published: (1960)

Transonic tunnel tests on a 6% thick, warped 55 sweptback-wing model /
by: Haines, A. B.
Published: (1965)

The load near the apex of a lifting swept wing in linearised subsonic flow /
by: Davies, Patricia J.
Published: (1973)

Flight measurements of the drag of a swept-wing aircraft (Hunter Mk. I) at Mach numbers up to 1.2, together with some measurements of lift-curve slope /
by: Andrews, Dougles Raymond
Published: (1966)

The calculation of the spanwise loading of sweptback wings with flaps or all-moving tips at subsonic speeds /
by: Brebner, G. G.
Published: (1967)

Measurements of the direct pitching-moment derivatives for three wing planforms at high subsonic speeds /
by: Bratt, J. B.
Published: (1965)

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

Wind-tunnel tests at low speed of swept and yawed wings having various plan forms /
by: Purser, Paul E.
Published: (1951)

A study of the effect of leading-edge modifications on the flow over a 50-deg sweptback wing at transonic speeds /
by: Rogers, E. W. E.
Published: (1962)

An approximate integral method for calculating the incompressible laminar boundary layer on an infinite swept wing on which velocity and suction distribution are arbitrary /
by: Pinsent, H. G.
Published: (1962)

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)

An analysis of the flow over two 45-deg sweptback wings at high subsonic speeds, and comparison with theory /
by: Cook, R.
Published: (1961)

Wind-tunnel investigation of a large-scale 25° swept-wing jet transport model with an external blowing triple-slotted flap /
by: Aoyagi, Kiyoshi, et al.
Published: (1973)

The lift and stalling characteristics of a 35 deg. swept back wing designed to have identical chordwise pressure distributions at all spanwise stations when near maximum lift /
by: Woodward, D. S.
Published: (1973)

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)

The drag of infite [as printed] swept wings : with an addendum /
by: Cooke, J. C. (John Caister)
Published: (1969)

Flight tests on the Short SB5 with 60 degrees sweepback and low tailplane /
by: Staples, K. J.
Published: (1969)

Experimental investigation of ice accretion effects on a swept wing : final report.
Published: (2005)

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

Effect of wing bend on the experimental force and moment characteristics of an oblique wing /
by: Hopkins, Edward J., et al.
Published: (1976)

Effect of drooped-nose flaps on the experimental force and moment characteristics of an oblique wing /
by: Hopkins, Edward J., et al.
Published: (1976)

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)

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

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

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)

Effect of Kruger nose flaps on the experimental force and moment characteristics of an oblique wing /
by: Hopkins, Edward J., et al.
Published: (1976)

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

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

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

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

Variable sweep : a case history of multiple re-innovation /
by: Perry, Robert, 1925-
Published: (1966)

Effect of Kruger nose flaps on the experimental force and moment characteristics of an oblique wing /
by: Hopkins, Edward J., et al.
Published: (1976)