Low-speed tunnel tests of an aspect-ratio 9 jet-flap model, with ground simulation by moving-belt rig /

Flight measurements of ground effect on the lift and pitching moment of a large transport aircraft (Comet 3B) and comparison with wind tunnel and other data /
by: O'Leary, C. O.
Published: (1969)

Tests on the loss of vertical jet thrust due to ground effect on two simple VTOL planforms : with particular reference to the short SC b1 s aircraft /
by: Wyatt, L. A.
Published: (1963)

Air cushion vehicles, transportation of the future.
Published: (1962)

Low-speed wind-tunnel measurements of damping in yaw (n[psi]) on an A.R. 9 jet-flap complete model /
by: Cox, A. P.
Published: (1967)

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)

Proceedings.

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)

A moving-belt rig for ground simulation in low-speed wind tunnels /
by: Butler, S. F. J.
Published: (1967)

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

A flight-dynamic helicopter mathematical model with a single flap-lag-torsion main rotor /
by: Takahashi, Marc D.
Published: (1990)

A control-surface oscillatory derivative rig for use with half-models in high-speed wind tunnels /
by: Wight, K. C., et al.
Published: (1976)

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

Ground-Cushion Phenomenon : hearings before the United States House Committee on Science and Astronautics, Eighty-Sixth Congress, first session, on Apr. 13-15, 1959.
Published: (1959)

An evaluation of the method for determining the Whitham F-function using distributions of downwash and sidewash angles /
by: Mendoza, Joel P., et al.
Published: (1976)

A theoretical and experimental investigation of the external-flow, jet-augmented flap /
by: Ashill, P. R.
Published: (1975)

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)

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

Air cushion landing systems ; proceedings /

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

Elevation of a Full-Thickness Mucoperiosteal Flap Alone Accelerates Orthodontic Tooth Movement /
by: Owen, Kelly Martinez
Published: (2015)

The flapping behaviour of a helicopter rotor at high tip-speed ratios /
by: Wilde, Ernest
Published: (1966)

Wall corrections to longitudinal components measured on wind-tunnel models with tails /
by: Lovell, D. A.
Published: (1969)

Two-dimensional low-speed tunnel tests on the NACA 0012 section, including measurements made during pitching oscillations at the stall /
by: Moss, G. F., et al.
Published: (1971)

Measurement of turbulence in the Liverpool University turbomachinery wind tunnels and compressor /
by: Shaw, R. (Ronald), 1924-, et al.
Published: (1966)

An application of fast frequency-sweep excitation to the measurement of sub-critical response of a low speed wind tunnel model /
by: Skingle, C. W. (Colin William)
Published: (1976)

An analogue computer for on-line correction of wind-tunnel force and moment data /
by: Pecover, B. E.
Published: (1967)

Super VC 10 cruise drag-A wind-tunnel investigation /
by: Taylor, C. R.
Published: (1970)

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

Wind tunnel flutter tests at subsonic speeds on a half-wing with a fan engine nacelle /
by: Drane, D. A., et al.
Published: (1976)

Finite difference solutions for an unsteady interference parameter in slotted wind tunnels /
by: Rushton, K. R.
Published: (1969)

Analytic determination of the axial velocity through a propeller moving perpendicular to its axis /
by: Mandl, P.
Published: (1960)

Advanced hypersonic test facilities /
Published: (2002)

Some results of wind-tunnel tests on an aerofoil section (NPL 9510) combining a 'peaky' upper surface-pressure distribution with rear loading /
by: Hall, D. J. (Aerospace engineer), et al.
Published: (1974)

Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration /
by: Campbell, Bryan A.
Published: (1999)

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)