Experiments at M b0 s= 4.03 on two families of pressure-plotting wing-and-half-cone combinations /

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)

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)

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

Further experimental investigation of the characteristics of cambered gothic wings at Mach numbers from 0.4 to 2.0 /
by: Squire, Leonard Charles
Published: (1963)

An experimental and theoretical comparison at M=4 of the lift-to-drag ratio of some possible aircraft shapes /
by: Brown, C. S. (Charles Scorer)
Published: (1969)

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

Measurement of the pitching-moment derivatives for rigid tapered wings of hexagonal planform oscillating in supersonic flow /
by: Woodgate, L.
Published: (1962)

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

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)

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

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

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)

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

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

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)

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)

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

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

The effect of combined boundary-layer suction and base bleed on the drag of a 10 degree cone at M=2.58 /
by: Goldsmith, E. L.
Published: (1970)

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)

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

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)

A free-flight investigation into the effect of body shaping on the zero-lift drag of a wing-body combination at transonic and supersonic speeds /
by: Hamilton, J. A.
Published: (1961)

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)

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

Tables of supersonic symmetrical flow around right circular cones : with and without the addition of heat at the wave /
by: Bartlett, Ronald Stanley
Published: (1968)

On the prediction of base pressure on two-dimensional supersonic turbulent flow /
by: Roberts, J. B. (Writer on aerodynamics)
Published: (1966)

The pressure-drag due to blunt leading edges on two-dimensional aerofoils : at transonic and low supersonic speeds /
by: Graham, William James
Published: (1967)

A new probe for the direct measurement of stagnation pressure in supersonic flow /
by: Goodyer, M. J.
Published: (1975)

The velocity potential on triangular and related wings with subsonic leading edges oscillating harmonically in supersonic flow /
by: Davies, David Eric
Published: (1961)

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)

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

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

Calculation of subsonic flutter derivatives for an arrowhead wing with control surfaces /
by: Lehrian, Doris E.
Published: (1969)

Inflated mobile lifting structures: analysis of membrane construction and design optimisation for oval planforms /
by: Brown, I. S. H.
Published: (1964)