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

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)

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

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

Boundary-layer drag of bi-convex wing sections with heat transfer at supersonic speeds /
by: Luxton, R. E.
Published: (1965)

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)

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)

Turbulent boundary layer theory and its application to blade profile design /
by: Smith, D. J. L.
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)

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

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)

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

The longitudinal characteristics of three slender 'mild ogee' wings at mach numbers from 0.4 to 2.0 /
by: Mabey, Dennis G.
Published: (1968)

The pressure distribution at zero lift on a slender delta wing at transonic speeds /
by: Firmin, Michael Charles Peter, 1929-
Published: (1968)

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

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)

An experimental investigation of propfan installations on an unsewpt supercritical wing at transonic Mach numbers /
by: Bartlett, Glynn R.
Published: (1985)

Experimental investigation of the positions of the leading-edge vortices above slender delta wings with various rhombic cross-sections in subsonic conical flow /
by: Kirkpatrick, David L. I.
Published: (1967)

Flight velocity effects on exhaust noise of a wedge nozzle installed on an underwing nacelle on an F-106 airplane /
by: Burley, Richard R.
Published: (1976)

Supercritical wing sections II : a handbook /
Published: (1975)

Wind tunnel studies of leading edge separation phenomena on a quarter scale model of the outer panel of the Handley Page 'Victor' wing : with and without nose droop /
by: Wallis, R. Allan
Published: (1967)

A theory of supercritical wing sections : with computer programs and examples /
by: Bauer, Frances
Published: (1972)

Experimental investigation of the effect of trailing-edge sweepback on the subsonic longitudinal characteristics of slender wings, by D. L. I. Kirkpatrick and A. G. Hepworth.
by: Kirkpatrick, David L. I.
Published: (1970)

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

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

Comparison of seven wing buffet boundaries measured in wind tunnels and in flight /
by: Mabey, Dennis G.
Published: (1966)

A theoretical investigation for delta wings with leading-edge separation at low speeds /
by: Nangia, R. K.
Published: (1970)

Characteristics of aft-mounted all-moving rectangular control surfaces on a slender cruciform model at mach numbers from 0.6 to 2.8 /
by: Winter, Kenneth George
Published: (1968)

The design of axisymmetric cowls for podded nacelles for high by-pass ratio turbofan engines /
by: Langley, M. J.
Published: (1980)

The vortex of appendage-body junction flow control using suitable fillets /
by: Li, Ding
Published: (1995)

Delta wings with longitudinal camber at low speed /
by: Nangia, R. K.
Published: (1970)

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

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

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

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)

Engine airframe integration problems peculiar to aircraft configurations with nacelles mounted above the wing /
by: Löbert, G.
Published: (1968)