A flight study of the sidestep manoeuvre during landing /

Some observations on manoeuvre stability and longitudinal control /
by: Pinsker, W. J. G.
Published: (1973)

Some flight measurements of crosswind landings on a small delta aircraft (Avro 707A) /
by: Staples, K. J.
Published: (1967)

A piloted simulator study of the take-off manoeuvre of a large aircraft with and without a take-off director /
by: O'Leary, C. O.
Published: (1968)

A flight simulator for research into aircraft handling characteristics /
by: Perry, D. H. (David Howard)
Published: (1969)

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

Landing transition paths which optimise fuel, time, or distance for jet-lift VTOL transport aircraft in steep approaches /
by: Huntley, E.
Published: (1974)

Flight tests on the Short SB5 with 60 degrees sweepback and low tailplane /
by: Staples, K. J.
Published: (1969)

A wind-tunnel investigation of the directional and longitudinal stability of the Javelin aircraft at transonic speeds, including comparison with flight test results /
by: Sutton, E. P.
Published: (1965)

Flight tests of a hovering jet-lift aircraft : (Rolls-Royce Flying Bedstead) /
by: Illingworth, J. K. B.
Published: (1963)

A technique for the automatic, digital analysis of flight dynamic response data /
by: Waterfall, A. P.
Published: (1972)

Directional stability in flight with bank angle constraint as a condition defining a minimum acceptable value for n[superscript v] /
by: Pinsker, W. J. G.
Published: (1968)

The aerodynamic forces on an oscillating two-dimensional wing in accelerated supersonic flight /
by: Davies, Danny E.
Published: (1962)

Flight tests to investigate the dynamic lateral-stability characteristics of a 45-deg delta, cropped to give three aspect ratios /
by: Nethaway, J. E.
Published: (1962)

Flight measurements of the lift, longitudinal trim and drag of the Fairey Delta 2 at mach numbers up to 1.65 and comparisons with wind-tunnel results /
by: Rose, Robert
Published: (1969)

Variable stability and control tests on the S.C.1 aircraft in jet-borne flight, with particular reference to desirable VTOL flying qualities /
by: Illingworth, J. K. B.
Published: (1969)

Flight measurements of the elevator and aileron hinge-moment derivatives of the Fairey Delta 2 aircraft up to a Mach number of 1.6 and comparisons with wind-tunnel results /
by: Rose, Robert
Published: (1967)

A study of slender, cambered, conical wings by an electrical resistance network /
by: Ward, H. S.
Published: (1964)

Free-flight measurements of pressure and heat transfer on a blunt leading-edge caret wing at design and off-design mach numbers (M [infinity] =0.9 to 3.36) /
by: Greenwood, G.H
Published: (1971)

The calculation of the rotary lateral stability derivatives of a jet-flapped wing /
by: Thomas, H. H. B. M.
Published: (1962)

Flight measurements of the drag of a swept-wing aircraft (Hunter Mk. I) at Mach numbers up to 1.2, together with some measurements of lift-curve slope /
by: Andrews, Dougles Raymond
Published: (1966)

Measurements of the performance of a turbo-jet engine with reheat (Rolls Royce RA28R Avon) in high-speed flight and under simulated conditions in test beds /
by: Woodfield, Alan Anthony
Published: (1968)

Free-flight measurements of the transonic roll-damping characteristics of three related wings of aspect ratio 2.83 /
by: Turner, K. J.
Published: (1962)

Effects of longitudinal elastic camber on slender aircraft in steady symmetrical flight ; Parts I and II /
by: Taylor, A. S.
Published: (1966)

Experiments on a delta wing with jet-assisted lift /
by: Melbourne, W. H.
Published: (1962)

Flight determination of wing flow patterns and buffet boundaries for the Fairey Delta 2 aircraft at Mach numbers between 0.4 and 1.3 : and comparison with wind tunnel results /
by: Dee, F. W.
Published: (1967)

Low-speed wind-tunnel tests on a series of uncambered slender pointed wings with sharp edges /
by: Peckham, D. H.
Published: (1961)

The stability of an aircraft under automatic throttle control and the cross-coupling effects with elevator control /
by: Fry, D. E.
Published: (1963)

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)

The application of a parametric method of fatigue load measurement to wings : based on flight measurements on a Lightning Mk T5 /
by: Burns, Anne
Published: (1979)

Computation of the velocity field induced by a planar source distribution approximating a symmetrical non-lifting wing in subsonic flow /
by: Ledger, J. A.
Published: (1974)

The effect of variations in local gravity and of aircraft speed on the effective weight of aircraft in high performance cruise /
by: Pinsker, W. J. G.
Published: (1972)

An experimental investigation of the effect of planform shape on the subsonic longitudinal stability characteristics of slender wings /
by: Kirby, D. A. (Donald Allen), 1926-
Published: (1969)

A piloted simulator study of a slender-wing research aircraft (HP 115) /
by: McPherson, A.
Published: (1970)

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

A review of recent research on handling qualities, and its application to the handling problems of large aircraft /
by: Bisgood, P. L.
Published: (1967)

An experimental method for the study of the impact between a liquid drop and a surface moving at high speed /
by: Jenkins, D. C.
Published: (1961)