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 /

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)

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

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)

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

Phase averaged measurements of the coherent structure of a Mach number 0.6 jet /
by: Emami, Saied
Published: (1983)

Phase averaged measurements of the coherent structure of a Mach number 0.6 jet /
by: Emami, Saied, 1956-
Published: (1983)

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

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

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)

Independent effects of Reynolds number and Mach number on aerodynamics of an iced swept wing /
by: Broeren, Andy P.
Published: (2019)

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)

Comparison of theoretical and experimental steady wing loads on a space shuttle configuration at Mach numbers of 0.6 and 1.4 /
by: Preisser, John S.
Published: (1977)

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

Swept wing ice accretion modeling /
by: Potapczuk, Mark G.
Published: (1990)

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)

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

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)

Low-Reynolds number aerodynamics of an 8.9 percent scale semispan swept wing for assessment of icing effects /
by: Broeren, Andy P.
Published: (2017)

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

Experimental aerodynamic characteristics for slender bodies with thin wings and tail at angles of attack from 0 ̊to 58 ̊and Mach from 0.6 to 2.0 /
by: Jorgensen, Leland Howard, et al.
Published: (1976)

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)

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

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)

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

Applications of Ko displacement theory to the deformed shape predictions of the doubly-tapered Ikhana wing /
by: Ko, William L.
Published: (2009)

LWC and temperature effects on ice accretion formation on swept wings at glaze ice conditions /
by: Vargas, Mario (Aerospace researcher), et al.
Published: (2000)

Icing simulation research supporting the ice-accretion testing of large-scale swept-wing models /
by: Yadlin, Yoram
Published: (2018)

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

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

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)

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