Tests at M= 1.82 on an engine installation with boundary-layer diverter for a slender gothic wing /

Free-flight measurements of the incremental drag due to engine nacelles on a transonic swept-wing aircraft / by G.K. Hunt.
by: Hunt, G. K.
Published: (1967)

Low-speed wind-tunnel tests of a two-dimensional wing fitted with two plain differentially-deflected trailing-edge flaps /
by: McKie, John (Aerodynamicist)
Published: (1975)

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

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

Results and analysis of pressure measurements on two isolated slender wings and slender wing-body combinations at supersonic speeds /
by: Fellows, K. A.
Published: (1970)

Measurements of buffeting on slender wing models /
by: Mabey, Dennis G.
Published: (1967)

The prediction of boundary-layer behaviour and profile drag for infinite yawed wings.
by: Thompson, B. G. J., et al.
Published: (1974)

The prediction of boundary-layer behaviour and profile drag for infinite yawed wings.
by: Thompson, B. G. J.
Published: (1974)

The prediction of boundary-layer behaviour and profile drag for infinite yawed wings.
by: Thompson, B. G. J.
Published: (1974)

The dynamic stability derivatives of a slender wing : a comparison of theory with free-flight model tests at near-zero lift, M = 0.8 to 2.4 /
by: Turner, K. J.
Published: (1968)

Wind tunnel test of composite wing extensions : test number 8112 & 8115 /
by: Nicks, Oran W.
Published: (1982)

The calculation of three-dimensional turbulent boundary layers.
by: Cumpsty, N. A.
Published: (1970)

Thrust/drag analysis for a front fan nacelle having two separate co-axial exhaust streams /
by: Street, P. G.
Published: (1975)

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 test of a composite wing extension designed for a specific application : test number 8203 /
by: Nicks, Oran W.
Published: (1982)

Tests at a mach number of 2.0 on a rectangular twin-duct air intake with variable geometry : situated in the flow field of a slender wing /
by: Dobson, M. D.
Published: (1970)

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

Transonic wind tunnel test of a 14% thick oblique wing /
Published: (1990)

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

Low-speed wind-tunnel tests on a delta-wing aircraft model (S.R. 177) with blowing over the trailing-edge flaps and ailerons /
by: Butler, S. F. J.
Published: (1966)

Low-speed wind-tunnel measurements of the lift, drag and pitching moment on three symmetrical ogee-wing models and on a symmetrical slender wing-body model /
by: Kirby, D. A. (Donald Allen), 1926-
Published: (1966)

A method of correlating the ground effects on the longitudinal characteristics of slender wings /
by: Kirkpatrick, David L. I.
Published: (1970)

Boundary layer separation in aircraft aerodynamics : proceedings of the seminar held on 6 February 1997 in Delft dedicated to Professor J.L. van Ingen /
Published: (1997)

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

Calculation of the laminar boundary layer and prediction of transition on a sheared wing /
by: Beasley, J. A.
Published: (1976)

Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle /
by: Lamb, Milton
Published: (1985)

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)

Low-speed wind-tunnel tests of a number of fin configurations on a flat-plate gothic wing of unit aspect ratio /
by: Peckham, D. H.
Published: (1969)

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)

Investigation of the normal force characteristics of slender delta wings with various rhombic cross-sections in subsonic conical flow /
by: Kirkpatrick, David L. I.
Published: (1967)

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)

Measurements of secondary flow in the boundary layers of a 180 degree channel /
by: Patel, V. C. (Virendrakumar Chaturbhai)
Published: (1969)

Camber effects on the non-linear lift of slender wings with sharp leading edges /
by: Squire, Leonard Charles
Published: (1967)

The dynamic stability derivatives of a slender wing at zero and moderate lift : a comparison of theory with free-flight model tests, M = 0.8 to 2.0 /
by: Ross, A. Jean, et al.
Published: (1975)

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

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)