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)

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)

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

Proceedings.

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

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

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

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)

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

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

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

Air cushion landing systems ; proceedings /

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

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

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)

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

Advanced hypersonic test facilities /
Published: (2002)

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

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)

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

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)

Ground effect--theory and practice.
Published: (1937)

An aerodynamic analysis computer program and design notes for low speed wing flap systems /
by: Carlson, Harry W.
Published: (1983)

A technique for the wind tunnel simulation of store release at high speeds /
by: Beecham, L. J.
Published: (1966)

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)

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

Subsonic tests in free molecule flow on impact tube pressure probes having a wide range of tube lengths at angles of attack up to 90 ̊ /
by: Hughes, Peter C. (Peter Carlisle), 1940-
Published: (1965)

Characteristics of high-speed wind tunnels in the United Kingdom relevant to aeroelastic-model tests /
by: Irwin, C. A. K.
Published: (1967)

Fixed and flapping wing aerodynamics for micro air vechicle applications /
Published: (2002)

Interference effects at M=8.5 of wires and probes on the wake of a magnetically suspended rounded base cone /
by: Crane, John Frank William
Published: (1970)