The pressure distribution on two-dimensional wings near the ground /

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

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

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

N.P.L. aerofoil catalogue and bibliography /
by: Pankhurst, R. C.
Published: (1963)

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

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)

Design and test of a series of annular aerofoils /
by: Ryall, D. L.
Published: (1967)

A new series of low-drag aerofoils /
by: Nonweiler, T. R. F.
Published: (1971)

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)

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

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

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)

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 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)

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

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)

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)

An investigation of annular aerofoils for turbofan engine cowls /
by: Young, C.
Published: (1972)

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

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

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

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

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

Methods for analysis of two-dimensional airfoils, with subsonic and transonic applications /
by: Bennett, J. A.
Published: (1966)

Applied wing theory /
by: Reid, Elliott Gray
Published: (1932)

Wing theory /
by: Jones, Robert T. (Robert Thomas), 1910-1999
Published: (1990)

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

A thin wing in a compressible flow /
by: Krasilʹshchikova, E. A.
Published: (1982)

Basic wing and airfoil theory.
by: Pope, Alan, 1913-
Published: (1951)

Theory of wing sections : including a summary of airfoil data /
by: Abbott, Ira Herbert, 1906-
Published: (1959)

Theory of wing sections : including a summary of airfoil data /
by: Abbott, Ira Herbert, 1906-
Published: (1949)

An equivalence law relating three- and two-dimensional pressure distributions /
by: Lock, R. C.
Published: (1964)

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

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)