Strength and elastic response of symmetric angle-ply carbon fibre reinforced plastics /

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)

An extensive theoretical study of the ability of slender-wing aircraft to perform sidestep manoeuvres at approach speeds /
by: Tomlinson, Barry Nigel
Published: (1964)

The design of Michell optimum structures /
by: Chan, A. S. L.
Published: (1962)

On lifting bodies which contain two-dimensional supersonic flows /
by: Townend, L. H.
Published: (1964)

The relationship between upward accelerations and mean associated downward accelerations experienced by aircraft in manoeuvring flight /
by: Owen, E. Marjorie
Published: (1964)

A numerical method for calculating the pressure due to thickness on symmetrical wings at zero incidence in supersonic flow /
by: Eldridge, Robert Henry
Published: (1968)

Stress-concentration factors for rounded rectangular holes in infinite sheets /
by: Sobey, Albert J.
Published: (1965)

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)

Rolling-power tests on an elastic model wing (M-planform) in low-speed flow /
by: Gaukroger, D. R. (Donald Richard)
Published: (1964)

The longitudinal response of a flexible slender aircraft to random trubulence /
by: Huntley, E.
Published: (1967)

A theoretical investigation of the longitudinal stability, control and response characteristics of jet-flap aircraft /
by: Taylor, A. S.
Published: (1962)

Britain's greatest aircraft /
by: Jackson, Robert, 1941-
Published: (2007)

An investigation of the flow about a plane half-wing of cropped-delta planform and 6 per cent symmetrical section at stream Mach numbers between 0.8 and 1.41 /
by: Rogers, E. W. E.
Published: (1962)

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

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)

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)

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)

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

The dynamics of aircraft rotation and lift-off and its implications for tail clearance requirements, especially with large aircraft /
by: Pinsker, W. J. G.
Published: (1969)

On the elastic moduli of undirectional fibre reinforced composites /
by: Mansfield, Eric Harold, 1923-
Published: (1976)

The subcritical response and flutter of a slender wing model aircraft /
by: Payen, D. B.
Published: (1969)

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

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

Aileron control of small-aspect-ratio aircraft ; in particular, Delta aircraft /
by: Pinsker, W. J. G.
Published: (1960)

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 investigation of the feasibility of reshaping stick commands to improve hovering control of unstabilized jet-lift aircraft /
by: Wilson, R., Ph.D
Published: (1968)

The encyclopedia of Russian aircraft, 1875-1995 /
by: Gunston, Bill
Published: (1995)

Subsonic wind-tunnel tests on a crescent-winged aircraft, including tests of leading-edge droop designs and several tailplane heights /
by: Hall, C. N.
Published: (1961)

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

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

Interference problems on wing-fuselage combinations in inviscid, incompressible flow /
by: Weber, J.
Published: (1976)

Calculation of the response of a flexible aircraft to harmonic and discrete gusts by a transform method /
by: Mitchell, C. G. B.
Published: (1968)

The subcritical response and flutter of a swept-wing model /
by: Irwin, C. A. K.
Published: (1968)

Theoretical assessment of the general stability and gust response characteristics of STOL aircraft /
by: Pinsker, W. J. G.
Published: (1971)

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

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)