Further experimental investigation of the characteristics of cambered gothic wings at Mach numbers from 0.4 to 2.0 /

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

Wind tunnel tests of a wing fitted with a single lifting fan /
by: Gregory, Nigel
Published: (1967)

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

Analysis of the zero-lift wave drag measured on delta wings /
by: Weber, J.
Published: (1978)

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)

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

The lift and stalling characteristics of a 35 deg. swept back wing designed to have identical chordwise pressure distributions at all spanwise stations when near maximum lift /
by: Woodward, D. S.
Published: (1973)

Exploratory investigation of the effects of blowing from the leading edge of a delta wing /
by: Trebble, W. J. G.
Published: (1968)

Accuracy of downwash evaluation by Multhopp's lifting-surface theory /
by: Garner, Henry Clifford
Published: (1966)

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

Comparison of three methods for the evaluation of subsonic lifting-surface theory /
by: Garner, Henry Clifford
Published: (1969)

Camber effects on the non-linear lift of slender wings with sharp leading edges /
by: Squire, Leonard Charles
Published: (1967)

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)

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

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

The calculation of generalised forces on oscillating wings in supersonic flow by lifting surface theory /
by: Harris, G. Z.
Published: (1967)

The effect of forward speed on the inlet flow distribution and performance of a lifting fan installed in a wing /
by: Gregory, Nigel
Published: (1965)

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

Measurements of section pressure distribution at a mach number of 2.0 on a wing of 70 degrees sweep mounted on a waisted body /
by: Winter, K. G.
Published: (1971)

Algol 60 programme for Multhopp's low-frequency subsonic lifting-surface theory /
by: Garner, Henry Clifford
Published: (1968)

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)

The longitudinal characteristics of three slender 'mild ogee' wings at mach numbers from 0.4 to 2.0 /
by: Mabey, Dennis G.
Published: (1968)

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

Flow past conically-cambered slender delta wings with leading-edge separation /
by: Barsby, J. E.
Published: (1974)

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

An airfoil shape for efficient flight at supercritical Mach numbers /
by: Whitcomb, Richard T.
Published: (1965)

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)

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)

Wind tunnel tests on cambered wings of mild gothic planform : parts I and II /
by: Butterworth, P. J.
Published: (1978)

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)

Flutter characteristics of a wing carrying a flexibly mounted mass /
by: Gaukroger, D. R. (Donald Richard)
Published: (1963)

Pressure-plotting and force tests at Mach numbers up to 2.8 on an uncambered slender wing of p = 1/2, s/co = 1/4 ('Handley Page Ogee') /
by: Courtney, Adrian Laurence
Published: (1964)

Wind tunnel experiments on a lifting jet in a bluff body with and without wings /
by: Trebble, W. J. G.
Published: (1966)

Some observations of the flow over a deltawinged model with 55-deg leading-edge sweep, at Mach numbers between 04 and 18 /
by: Sutton, E. P.
Published: (1960)

Lifting surface theory for a rotating subsonic or transonic blade row /
by: Namba, M. (Masanobu), 1936-
Published: (1974)

An application of Flax's variational principle to lifting-surface theory /
by: Davies, Danny E.
Published: (1969)