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 /

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)

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

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)

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

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

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

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

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

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)

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 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)

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)

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

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

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

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

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)

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

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

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

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

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

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)

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

Measurement of the critical distance parameter against icing conditions on a NACA 0012 swept wing tip /
by: Vargas Meza, Mario
Published: (2011)

Aerodynamic classification of swept-wing ice accretion /
by: Broeren, Andy P., et al.
Published: (2013)

Dynamics and control of forward swept wing aircraft /
by: Schmidt, D. K. (David K.), et al.
Published: (1984)

Tollmien-Schlichting and Crossflow Instability Mode Selection on Swept Wings /
by: Feliciano, Jeppesen G
Published: (2023)

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

Swept-wing ice accretion characterization and aerodynamics /
by: Broeren, Andy P.
Published: (2013)