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) /

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)

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

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

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

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)

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)

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 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)

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)

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)

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

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)

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)

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

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

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

Receptivity studies on a swept-wing model /
by: Woodruff, Matthew Jeffery
Published: (2012)

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)

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)

Aerodynamic classification of swept-wing ice accretion /
by: Diebold, Jeff M., et al.
Published: (2013)

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)

Analysis of low-speed stall aerodynamics of a swept wing with laminar-flow glove /
by: Bui, Trong T.
Published: (2014)

Natural laminar flow flight experiments on a swept wing business jet- boundary layer stability analyses /
by: Rozendaal, R. A.
Published: (1986)

Aerodynamic Design for Swept-wing Laminar Flow /
by: Belisle, Michael Joseph
Published: (2014)

Further experimental investigation of the characteristics of cambered gothic wings at Mach numbers from 0.4 to 2.0 /
by: Squire, Leonard Charles
Published: (1963)

Leading-edge deflection optimization for a highly swept arrow-wing configuration /
by: Coe, Paul L., et al.
Published: (1980)