Calculation of stability derivatives for tapered wings of hexagonal planform oscillating in a supersonic stream /

Theoretical subsonic derivatives for an oscillating M-wing /
by: Garner, Henry Clifford
Published: (1961)

Measurements of the direct pitching oscillation derivatives for three cropped delta and three arrowhead planforms at subsonic and transonic speeds /
by: Miles, C. J. W.
Published: (1965)

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

An improved method for calculating generalised airforces on oscillating wings in subsonic flow /
by: Long, G.
Published: (1971)

Co-ordinated experimental and theoretical research on the oscillatory airforces for selected planforms at subsonic and supersonic speeds /
by: Woodcock, David Leon, 1922-
Published: (1969)

An experimental investigation of the subsonic longitudinal characteristics of five slender-wing models with gothic planforms /
by: Kirkpatrick, D. L. I.
Published: (1973)

Half-body and wing combinations in supersonic flow : a review of some principles and possibilities /
by: Goldsmith, E. L.
Published: (1968)

Comparative theoretical calculations of forces on oscillating wings through the transonic speed range /
by: Garner, Henry Clifford
Published: (1969)

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)

Pressure distribution on two wings with curved leading edges at supersonic speeds /
by: Narayan, K. Yegna
Published: (1974)

The calculation of the warp to produce a given load and the pressures due to a given thickness on thin slender wings in supersonic flow /
by: Smith, Jeremy H. B.
Published: (1967)

Part I: The flow pattern on a tapered swept-back wing at Mach numbers between 0.6 and 1.6. Part II: Experiments with a tapered swept-back wing of Warren 12 planform at Mach numbers between 0.6 and 1.6 /
by: Hall, Ian Murray
Published: (1962)

Some exact calculations of the lift and drag produced by a wedge in supersonic flow : either directly or by interference /
by: Roe, P. L.
Published: (1967)

Measurements of aerodynamic derivatives on a wing with a series of tip bodies /
by: Guyett, Peter Robert
Published: (1964)

Some calculations of the take-off behaviour of a slender-wing supersonic transport design constrained to follow a specified pitch-attitude time history /
by: Tomlinson, Barry Nigel
Published: (1967)

An experimental investigation at supersonic speeds of the characteristics of two gothic wings, one plane and one cambered /
by: Squire, Leonard Charles
Published: (1961)

Aerodynamic derivative measurements on a wing with a horn-balanced control surface /
by: Guyett, Peter Robert
Published: (1963)

Measurements of skin friction on a cambered delta wing at supersonic speeds /
by: Winter, Kenneth George
Published: (1967)

Evaluation of pressure distributions on thin wings with distorted control surfaces oscillating harmonically in linearised, compressible, subsonic flow /
by: Marchbank, W. R.
Published: (1976)

Theory of lifting surfaces oscillating at general frequencies in a subsonic stream /
by: Acum, Wilfred Ethelbert Aldred
Published: (1969)

An iterative method for calculation of the loading on a thin unswept wing /
by: Sells, C. C. L. (Christopher Cedric Lytton)
Published: (1973)

Measurements of the pitching-moment derivatives on a sharp-edged delta wing in incompressible flow /
by: Woodgate, L.
Published: (1964)

An experimental investigation of the transonic flow over an unswept wing of aspect ratio 3.5, taper ratio O. 5, with a 4 per cent biconvex section /
by: Scott-Wilson, J. B.
Published: (1961)

Measurements in low-speed flow of unsteady pressure distributions on a rectangular wing with an oscillating control surface /
by: Drane, D. A.
Published: (1976)

Calculation of the induced velocity field on and off the wing plane for a swept wing with given load distribution /
by: Sells, C. C. L. (Christopher Cedric Lytton)
Published: (1973)

A momentum analysis of lifting surfaces in inviscid supersonic flow /
by: Roe, P. L.
Published: (1969)

Calculations of the flow over thick, conical, slender wings with leading-edge separation /
by: Smith, J. H. B.
Published: (1972)

The theoretical treatment of slowly oscillating part-span control surfaces in subsonic flow /
by: Garner, Henry Clifford
Published: (1971)

Use of camber and twist to produce low-drag delta or swept-back wings, without leading-edge singularities, at supersonic speeds /
by: Roper, G. M.
Published: (1961)

Measurements of the direct pitching-moment derivatives for three wing planforms at high subsonic speeds /
by: Bratt, J. B.
Published: (1965)

The unsteady forces on finite wings in transient motion /
by: Dore, Barrie Dennis
Published: (1967)

Calculations of the effect of blowing from the leading edges of a slender delta wing /
by: Barsby, J. E.
Published: (1972)

The separated flows on slender wings in unsteady motion /
by: Lowson, M. V.
Published: (1967)

Iterative method for thick cambered wings in subcritical flow /
by: Sells, C. C. L. (Christopher Cedric Lytton)
Published: (1976)

Tests at subsonic and supersonic speeds on a slender cambered wing with fin, underwing engine nacelles and trailing-edge controls /
by: Isaacs, Donald
Published: (1969)

Combined flexure and torsion of a class of heated thin wings : a large-deflection analysis /
by: Mansfield, Eric Harold, 1923-
Published: (1961)