Low-speed wind-tunnel measurements of damping in yaw (n[psi]) on an A.R. 9 jet-flap complete model /

Balance measurements (excluding drag) on a delta wing aircraft at transonic speeds /
by: Shaw, M. M.
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)

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

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

Free-flight tests of vortex generator configurations at transonic speeds /
by: Edwards, J. B. W.
Published: (1966)

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)

The aerodynamics of jet flaps /
by: Williams, John, 1922-1994
Published: (1963)

The two-dimensional flow around a slotted flap /
by: Foster, D. N.
Published: (1971)

The aerodynamic effect of ground proximity on lateral control of slender aircraft in the landing approach /
by: Pinsker, W. J. G.
Published: (1971)

The lateral oscillation of slender aircraft /
by: Ross, A. Jean
Published: (1966)

High-speed flight propulsion systems /
Published: (1991)

A study of the effect of the wake of the main aerofoil of a Fowler-flap configuration on the lift of the flap /
by: Ashill, P. R.
Published: (1973)

A study of the effect of the wake of the main aerofoil of a Fowler-flap configuration on the lift of the flap /
by: Ashill, P. R.
Published: (1973)

Six-component low-speed tunnel tests of jet-flap complete models with variation of aspect ratio, dihedral, and sweepback, including the influence of ground proximity /
by: Butler, S. F. J.
Published: (1967)

Interim report on low-speed flight tests of a slender-wing research aircraft (Handley Page H. P. 115) /
by: Bisgood, P. L.
Published: (1966)

The vortex drag of a swept wing with part-span flaps /
by: Garner, Henry Clifford
Published: (1972)

Wind-tunnel investigation of a fowler flap and spoiler for an advanced general aviation wing /
by: Paulson, John W.
Published: (1976)

Low-speed wind-tunnel measurements of the oscillatory lateral aerodynamic derivatives of a BAC 221 model and comparison of results with similar Concorde and HP 115 Data /
by: O'Leary, C. O.
Published: (1971)

Civil aircraft airworthiness data recording programme : a study of normal operational landing performance on subsonic civil jet aircraft /
by: Hutton, G. B.
Published: (1974)

Short-cowl front-fan turbojets ; friction drag and wall-jet effects on cylindrical afterbodies /
by: Green, John Edward
Published: (1969)

A simulator investigation of rolling requirements for landing approach /
by: Barnes, A. G.
Published: (1969)

A survey of unsteady hypersonic flow problems /
by: Wood, B. M.
Published: (1966)

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)

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 calculation method for the two-dimensional turbulent flow over a slotted flap /
by: Irwin, H. P. A. H. (Hamlyn Peter Anthony Hugh), 1945-
Published: (1974)

An assessment of the importance of the residual flexibility of neglected modes in the dynamical analysis of deformable aircraft /
by: Taylor, A. S., et al.
Published: (1976)

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

Measurement of the yawing moment of inertia of an aircraft (HP 115) in flight /
by: Poulter, R. L.
Published: (1972)

Flight and tunnel measurements of pressure fluctuations on the upper surface of the wing of a Venom aircraft with a sharpened leading-edge /
by: Rose, R. (Robert), et al.
Published: (1969)

Free-flight model dynamic stability measurements on a 'not-so slender' wing/fin combination at zero and small lift, M = 0.8 to 2.0 /
by: Greenwood, G. H., et al.
Published: (1975)

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)

Effect of aerodynamic uncertainties on unconventional lateral control at high angle of attack /
by: Eller, Bob Gensen, 1962-
Published: (1987)

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)

Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds /
by: Plentovich, Elizabeth B.
Published: (1991)