Design and test of a series of annular aerofoils /

Force and moment coefficients for vibrating aerofoils in cascade /
by: Whitehead, D. S. (Denis Sword)
Published: (1962)

Forces on aerofoils with both incidence and forward speed varying /
by: Randall, D. G.
Published: (1965)

The aerodynamic noise of a slot in an aerofoil /
by: Howe, M. S.
Published: (1978)

The two-dimensional characteristics of a 12·2% thick RAE 100 aerofoil section /
by: Woodward, D. S.
Published: (1971)

Measurement of pitching-moment derivatives for aerofoils oscillating in two-dimensional supersonic flow /
by: Scruton, C.
Published: (1962)

Lift due to interference between an aerofoil and an external non-lifting body /
by: Neumark, S.
Published: (1965)

Measurements of pitching-moment derivatives for blunt-nosed aerofoils oscillating in two-dimensional supersonic flow /
by: Pugh, P. G.
Published: (1963)

Aerodynamic data for three supercritical aerofoils, RAE (NPL 9515 and 9530, and RAE 9550 : parts I and II /
by: Fulker, J. L.
Published: (1978)

Experiments with biconvex and double-wedge aerofoils in low-density, supersonic flow /
by: Rogers, E. W. E.
Published: (1970)

A numerical solution of the analysis and design problems for the flow past one or more aerofoils or cascades /
by: Wilkinson, David Henry
Published: (1968)

Low-speed aerodynamic characteristics of NACA 0012 aerofoil section, including the effects of upper-surface roughness simulating hoar frost /
by: Gregory, N. (Nigel)
Published: (1973)

Estimates of the lift reduction due to boundary layer on two-dimensional aerofoils /
by: Beasley, J. A.
Published: (1967)

An extension to the method of Garabedian and Korn for the calculation of transonic flow past an aerofoil to include the effects of a boundary layer and wake /
by: Collyer, M. R.
Published: (1978)

An analysis of the subsonic flow past symmetrical blunt-trailing-edge aerofoil sections at zero incidence, in the absence of a vortex street /
by: Nash, John F.
Published: (1966)

Boundary-layer suction to eliminate corner separation in cascades of aerofoils /
by: Peacock, Roy E.
Published: (1971)

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

The pressure distribution on two-dimensional wings near the ground /
by: Bagley, John Arthur
Published: (1961)

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)

The elements of aerofoil and airscrew theory /
by: Glauert, H. (Hermann), 1892-1934
Published: (1943)

The elements of aerofoil and airscrew theory /
by: Glauert, H. (Hermann), 1892-1934
Published: (1983)

Experiments at M = 1.41 on a thin, conically-cambered elliptic cone of 30 semi-vertex angle /
by: Rogers, E. W. E.

A review of research on two-dimensional base flow /
by: Nash, John F.
Published: (1963)

The use of conical camber to produce flow attachment at the leading edge of a delta wing and to minimize life-dependent drag at sonic and supersonic speeds /
by: Smith, Jeremy H. B.
Published: (1963)

An analysis of two-dimensional turbulent base flow : including the effect of the approaching boundary layer /
by: Nash, John F.
Published: (1963)

Tip-clearance flow and losses for an isolated compressor blade /
by: Lakshminarayana, B.
Published: (1963)

The calculation of sub-critical pressure distributions on symmetric aerofoils at zero incidence /
by: Wilby, P. G.
Published: (1968)

Low speed wind tunnel tests on a series of rectangular wings of varying aspect ratio and aerofoil section /
by: Brebner, G. G.
Published: (1967)

Effects of longitudinal elastic camber on slender aircraft in steady symmetrical flight ; Parts I and II /
by: Taylor, A. S.
Published: (1966)

The pressure drag of an aerofoil with six different round leading edges, at transonic and low supersonic speeds /
by: Wilby, P. G.
Published: (1967)

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

Analysis of experimental data for a 21% thick natural laminar flow airfoil, NAE 68-060-21:1 = Analyse de données expérimentals d'un profil aérodynamique à écoulement laminaire naturel, NAE 68-060-21:1, d'une épaisseur de 21% /
by: Jones, D. J.
Published: (1985)

Airfoil design and data /
by: Eppler, Richard
Published: (1990)

Wing theory /
by: Robinson, Abraham, Ph.D
Published: (1956)

A theoretical study of annular supersonic nozzles /
by: Lord, W. T.
Published: (1961)

Design of a symmetrical section with specified pressure distribution /
by: Sells, C. C. L. (Christopher Cedric Lytton)
Published: (1969)

Further studies on the 21% thick, supercritical NLF airfoil NAE 68-060-21:1 = Études supplémentaires du profil NLF supercritique NAE 68-060-21:1 à épaisseur de 21% /
by: Khalid, M.
Published: (1986)