Approximate formulae for the lift and drag of wedge aerofoil sections at high supersonic speeds /

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

The nature, development and effect of the viscous flow around an aerofoil with high - lift devices /
by: Foster, D. N., et al.
Published: (1974)

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

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

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

Measurements of pressure distribution and shock-wave shape on power-law bodies at a mach number of 6.85 /
by: Peckham, D. H.
Published: (1967)

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

A two-dimensional aerofoil oscillating at low frequencies in high subsonic flow /
by: Nixon, David, 1947-
Published: (1974)

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

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)

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)

A parametric study of the use of nose blunting to reduce the supersonic wave drag of forebodies /
by: Pugh, P. G., et al.
Published: (1974)

Aerodynamic characteristics of NPL 9626 and NPL 9627, futher aerofoils designed for helicopter rotor use /
by: Wilby, P. G., et al.
Published: (1973)

The lift and drag characteristics of caret wings at Mach numbers between 5 and 10 /
by: Collingbourne, J. R.
Published: (1967)

High subsonic flow past a steady two-dimensional aerofoil /
by: Nixon, David, 1947-, et al.
Published: (1974)

Drag measurements on a series of afterbodies at transonic speeds showing the effect of sting interference /
by: Kurn, A. G.
Published: (1968)

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

Some comments on the conditions in a local supersonic flow region /
by: Moulden, Trevor H.
Published: (1968)

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

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

Experimental investigation of the effect of trailing-edge sweepback on the subsonic longitudinal characteristics of slender wings, by D. L. I. Kirkpatrick and A. G. Hepworth.
by: Kirkpatrick, David L. I.
Published: (1970)

Comparison between dynamic stability boundaries for NPL 9615 and NACA 0012 aerofoils pitching about the quarter-chord /
by: Moore, A. W. (Alan William), et al.
Published: (1974)

On the influence of camber and non-planar vortex wake on wing characteristics in ground effect /
by: Maskew, B.
Published: (1973)

Gun tunnel measurements of lift : drag and pitching moment on a 20 p0 scone, a flat delta and caret delta wing at a mach number of 8.3 /
by: Opatowski, T.
Published: (1967)

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)

Developments in high-speed-vehicle propusion systems /
Published: (1996)

Measurement of the internal drag of air breathing installations on slender wing-body combinations at supersonic speeds /
by: Britton, J. W.
Published: (1967)

Afterbody drag measurement at transonic speeds on a series of twin and single jet afterbodies terminating at the jet-exit /
by: Pozniak, O. M.
Published: (1973)

Some results of wind-tunnel tests on an aerofoil section (NPL 9510) combining a 'peaky' upper surface-pressure distribution with rear loading /
by: Hall, D. J. (Aerospace engineer), et al.
Published: (1974)

Experimental study of lift-enhancing tabs on a two-element airfoil /
by: Storms, Bruce L., et al.
Published: (1998)

Measurements of pressure fluctuations and skin friction on the upper surface of a slender wing at lift (M=0.8 to 2.0) /
by: Turner, K. J.
Published: (1968)

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

High-speed flight propulsion systems /
Published: (1991)

Applications of circulation control technologies /
Published: (2006)

Numerical solutions of hypersonic near-wake flow by the particle-in cell method /
by: Crane, Robert Ian
Published: (1970)

Thrust and drag : its prediction and verification /
Published: (1985)