Cover Image

Applications of circulation control technologies /

Show other versions (1)

Bibliographic Details
Other Authors:	Joslin, R. D. (Ronald Douglas), 1963-, Jones, Gregory S.
Format:	Book
Language:	English
Published:	Reston, VA : American Institute of Aeronautics and Astronautics, [2006]
Series:	Progress in astronautics and aeronautics ; v. 214.
Subjects:	Aerodynamics. Aerofoils.

Similar Items

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

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

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

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

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

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

Application of a variational method in plane compressible flow calculation /
by: Rasmussen, H., 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 characteristics of a family of rooftop aerofoils designed at their drag-rise condition in viscous, compressible flow.
by: Thompson, B. G. J., et al.
Published: (1975)

The characteristics of a family of rooftop aerofoils designed at their drag-rise condition in viscous, compressible flow.
by: Thompson, B. G. J., et al.
Published: (1975)

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)

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

NPL 9615 and NACA 0012 : a comparison of aerodynamic data /
by: Gregory, N., et al.
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)

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)

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

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

Applications of circulation control technologies /
Published: (2006)

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

Progress report on observations of three-dimensional flow patterns obtained during stall development on aerofoils, and on the problem of measuring two-dimensional characteristics /
by: Gregory, N.
Published: (1971)

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)

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

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)

Planar incompressible flow over an aerofoil and its wake /
by: Smith, F. T. (Frank T.), 1948-
Published: (1976)

Delta wings with longitudinal camber at low speed /
by: Nangia, R. K.
Published: (1970)

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)

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

Influence of the transonic doublet in the farfield of a lofting airfoil = Influence du doublet transsonique sur le champ d'écoulement à l'infini d'un profil portant /
by: Mokry, M.
Published: (1993)

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

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)

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 drag of two annular aerofoils /
by: Young, C.
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)

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

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

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

Analysis of low-speed unsteady airfoil flows /
Published: (2005)

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

Skin friction measurements for two relatively thick airfoil at high reynolds number = Mesures du frottement sur deux profils aérodynamiques assez épais à nombres de reynolds élevés /
by: Elfstrom, G. M.
Published: (1984)