An experimental and theoretical comparison at M=4 of the lift-to-drag ratio of some possible aircraft shapes /

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)

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

Numerical methods for calculating the zero-lift wave drag and the lift-dependent wave drag of slender wings /
by: Weber, J.
Published: (1961)

Experiments at M b0 s= 4.03 on two families of pressure-plotting wing-and-half-cone combinations /
by: Rogers, E. W. E.
Published: (1967)

Approximate formulae for the lift and drag of wedge aerofoil sections at high supersonic speeds /
by: Squire, Leonard Charles
Published: (1966)

On the design of wing-body combinations of low zero-lift drag rise at transonic speeds /
by: Lord, W. T.
Published: (1962)

Some notes on the zero-lift wave drag of slender wings with unswept trailing edge /
by: Weber, J.
Published: (1961)

Theoretical analysis of fluctuating lift on the rotor of an axial turbomachine /
by: Henderson, R. E.
Published: (1972)

Minimum drag surfaces of given lift which support two-dimensional supersonic flow fields /
by: Pike, Jack, 1937-
Published: (1968)

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)

The formulation of an influence-coefficient method for determining static aeroelastic effects : and its application to a slender aircraft in symmetric flight at M = 2.2 /
by: Taylor, A. S.
Published: (1969)

On the numerical evaluation of the drag integral.
by: Eminton, Evelyn
Published: (1963)

An experimental investigation of the influence of base bleed on the base drag of various propelling nozzle configurations /
by: Roberts, J. B. (Writer on aerodynamics)
Published: (1967)

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

A theoretical study of height control in flight close to the ground as affected by elevator lift and cockpit position /
by: Pinsker, W. J. G.
Published: (1971)

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

Numerical solutions of oscillatory lift interference /
by: Rushton, K. R.
Published: (1972)

Theoretical analysis of a gust alleviator used on a 'Lancaster' aircraft and comparison with experiment /
by: Zbrożek, J. K.
Published: (1963)

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

The effect of steady tailplane lift on the subcritical response of a subsonic t-tail flutter model /
by: McCue, D. J.
Published: (1971)

An analysis of the drag of two annular aerofoils /
by: Young, C.
Published: (1973)

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

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

The use of a deep electrolytic tank as a lifting-surface calculator /
by: Ward, H. S.
Published: (1963)

Notes on the approximate solution of lifting-surface theory used in the R.A.E. standard method /
by: Weber, J.
Published: (1974)

The variation of profile drag with Mach number up to the critical value : a comparison of recent predictions with early flight and wind-tunnel measurements and a comment on an earlier prediction,cby J. Osborne.
by: Osborne, John
Published: (1968)

An experimental assessment of the possibility of damage to leaded windows by sonic bangs /
by: Hunt, F. L.
Published: (1973)

Boundary layer bleed drag at supersonic speeds /
by: Goldsmith, E. L.
Published: (1968)

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

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

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

Mercury programmes for lifting surface theory calculations on wings oscillating in supersonic flow /
by: Harris, G. Z.
Published: (1966)

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

A flight investigation of the spanwise lift requirements of a helicopter rotor blade /
by: Riley, M. J.
Published: (1978)