An analysis of the flow over two 45-deg sweptback wings at high subsonic speeds, and comparison with theory /

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)

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)

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

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

Measurements of control-surface oscillatory derivatives on a sweptback, tapered model wing in two transonic tunnels /
by: Lambourne, N. C.
Published: (1977)

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

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)

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)

Low-speed wind-tunnel tests on the characteristics of leading-edge air intakes in swept wings /
by: Seddon, J.
Published: (1964)

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)

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)

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)

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

10-ft x 7-ft tunnel tests up to M = 0.94 of nose droop and a blunt-nosed NACA 3-00 type section on a 7 1/2 per cent thick 50 deg swept wing /
by: Courtney, Adrian Laurence
Published: (1961)

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)

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)

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

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

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

Boundary layer relaminarization device : patent application.
Published: (1992)

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

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

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

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

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

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

Wind tunnel investigation of jet interference for underwing installation of high bypass ratio engines /
by: Raney, Derek John
Published: (1969)

Some observations of the flow over a deltawinged model with 55-deg leading-edge sweep, at Mach numbers between 04 and 18 /
by: Sutton, E. P.
Published: (1960)

Interference problems on wing-fuselage combinations in inviscid, incompressible flow /
by: Weber, J.
Published: (1976)

Theoretical subsonic derivatives for an oscillating M-wing /
by: Garner, Henry Clifford
Published: (1961)

Pressure distribution and surface flow on 5% and 9% thick wings with curved tip and 60 sweepback /
by: Garner, Henry Clifford
Published: (1962)

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

Subsonic flow investigations on a cranked wing designed for high maneuverability /
by: Rao, Dhanvada M.
Published: (1986)

Experiments on two-dimensional base flow at subsonic and transonic speeds /
by: Nash, John F.
Published: (1967)

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

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)