Supersonic laminar boundary layers on cones /
| Main Author: | Cooke, J. C. (John Caister) |
|---|---|
| Format: | Book |
| Language: | English |
| Published: |
London :
H.M. Stationery Off,
1969.
|
| Series: | Current papers (Aeronautical Research Council (Great Britain)) ;
no. 1063. |
| Subjects: |
Similar Items
Leading edge effects on caret wings /
by: Cooke, J. C. (John Caister)
Published: (1968)
by: Cooke, J. C. (John Caister)
Published: (1968)
The use of air injection to prevent separation of the turbulent boundary layer in supersonic flow /
by: Peake, D. J.
Published: (1967)
by: Peake, D. J.
Published: (1967)
A prediction method for pressure distributions on compression surfaces of conical bodies at supersonic speeds /
by: Larcombe, M. J.
Published: (1974)
by: Larcombe, M. J.
Published: (1974)
Some studies of pressure distributions on the windward surfaces of conical bodies at high supersonic speeds /
by: Akers, Arthur
Published: (1966)
by: Akers, Arthur
Published: (1966)
Boundary layer bleed drag at supersonic speeds /
by: Goldsmith, E. L.
Published: (1968)
by: Goldsmith, E. L.
Published: (1968)
Effects of suction on the interaction between shock wave and boundary layer at a compression corner /
by: Tanner, L. H.
Published: (1970)
by: Tanner, L. H.
Published: (1970)
The correlation and prediction of pressure distributions on compression surfaces of sharp-edged conical bodies at high supersonic speeds /
by: Larcombe, M. J.
Published: (1969)
by: Larcombe, M. J.
Published: (1969)
Comparison of laminar and turbulent cone boundary layer flow with and without pressure gradient /
by: Graber, B. C.
Published: (1967)
by: Graber, B. C.
Published: (1967)
The effect of combined boundary-layer suction and base bleed on the drag of a 10 degree cone at M=2.58 /
by: Goldsmith, E. L.
Published: (1970)
by: Goldsmith, E. L.
Published: (1970)
Simple theoretical and experimental studies of the flow through a three-shock system in a corner /
by: Eminton, E.
Published: (1966)
by: Eminton, E.
Published: (1966)
The isobars in boundary layers at supersonic speeds /
by: Myring, D. F.
Published: (1967)
by: Myring, D. F.
Published: (1967)
The laminar boundary layer on an inclined cone /
by: Cooke, J. C. (John Caister)
Published: (1967)
by: Cooke, J. C. (John Caister)
Published: (1967)
Measurements of secondary loss in a model turbine with variable inlet boundary layer /
by: Denton, John D., et al.
Published: (1975)
by: Denton, John D., et al.
Published: (1975)
Evaluation of a technique to generate artificially thickened boundary layers in supersonic and hypersonic flows /
Published: (1991)
Published: (1991)
Viscous drag reduction in boundary layers /
Published: (1990)
Published: (1990)
Forces on cone cylinders at M=3.98 /
by: Moore, K. C.
Published: (1968)
by: Moore, K. C.
Published: (1968)
The use of surface pitot tubes as skin-friction meters at supersonic speeds /
by: Smith, K. G.
Published: (1964)
by: Smith, K. G.
Published: (1964)
The calculation of the pressure distribution on a thick cambered aerofoil at subsonic speeds including the effects of the boundary layer /
by: Powell, B. J
Published: (1968)
by: Powell, B. J
Published: (1968)
The calculation of momentum thickness in a turbulent boundary layer at mach numbers up to unity /
by: Nash, John F.
Published: (1967)
by: Nash, John F.
Published: (1967)
Feasibility and benefits of laminar flow control on supersonic cruise airplanes /
by: Powell, A. G.
Published: (1989)
by: Powell, A. G.
Published: (1989)
Feasibility and benefits of laminar flow control on supersonic cruise airplanes /
by: Powell, A. G.
Published: (1989)
by: Powell, A. G.
Published: (1989)
A note on skin-friction laws for the incompressible turbulent boundary layer /
by: Nash, John F.
Published: (1966)
by: Nash, John F.
Published: (1966)
The prediction of boundary-layer behaviour and profile drag for infinite yawed wings.
by: Thompson, B. G. J.
Published: (1974)
by: Thompson, B. G. J.
Published: (1974)
The prediction of boundary-layer behaviour and profile drag for infinite yawed wings.
by: Thompson, B. G. J.
Published: (1974)
by: Thompson, B. G. J.
Published: (1974)
The distribution of a wall pressure rise in a turbulent boundary layer /
by: Herd, R. J.
Published: (1967)
by: Herd, R. J.
Published: (1967)
The prediction of boundary-layer behaviour and profile drag for infinite yawed wings.
by: Thompson, B. G. J., et al.
Published: (1974)
by: Thompson, B. G. J., et al.
Published: (1974)
Transverse curvature effects in flows along corners and on wavy walls /
by: Gersten, K.
Published: (1972)
by: Gersten, K.
Published: (1972)
Some mutual interference effects between a 5.7 cone and sonic-leading-edge delta wing at M..-2.49 /
by: Goldsmith, E. L.
Published: (1967)
by: Goldsmith, E. L.
Published: (1967)
Some comments on the conditions in a local supersonic flow region /
by: Moulden, Trevor H.
Published: (1968)
by: Moulden, Trevor H.
Published: (1968)
Investigation of materials for boundary layer control in a supersonic wind tunnel /
by: Braafladt, Alexander C., et al.
Published: (2013)
by: Braafladt, Alexander C., et al.
Published: (2013)
Approximate calculation of three-dimensional laminar boundary layers /
by: Cooke, J. C. (John Caister)
Published: (1961)
by: Cooke, J. C. (John Caister)
Published: (1961)
Secondary instability of stationary crossflow vortices in Mach 6 boundary layer over a circular cone /
by: Li, Fei
Published: (2015)
by: Li, Fei
Published: (2015)
Turbulent-boundary layer behaviour and the auxiliary equation /
by: Nash, John F.
Published: (1966)
by: Nash, John F.
Published: (1966)
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)
by: Pugh, P. G., et al.
Published: (1974)
Supersonic flutter derivatives for a series of swept and cropped delta wings /
by: Harris, G. Z.
Published: (1967)
by: Harris, G. Z.
Published: (1967)
Boundary-layer pressure fluctuations at high Reynolds numbers on a second free-flight test vehicle /
by: Roberts, D. R.
Published: (1974)
by: Roberts, D. R.
Published: (1974)
Analysis of hinge moment data for rectangular and near rectangular trailing edge controls at supersonic and transonic speeds /
by: Isaacs, Donald
Published: (1966)
by: Isaacs, Donald
Published: (1966)
Calculation of compressible turbulent boundary layer on a flat plate /
by: Patankar, Suhas V., 1941-
Published: (1969)
by: Patankar, Suhas V., 1941-
Published: (1969)
A turbulent skin-friction law for use at subsonic and transonic speeds /
by: Nash, John F.
Published: (1967)
by: Nash, John F.
Published: (1967)
Supersonic turbulent boundary layers with periodic mechanical non-equilibrium /
by: Ekoto, Isaac Wesley, 1979-
Published: (2007)
by: Ekoto, Isaac Wesley, 1979-
Published: (2007)