Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by
Crossref.
Bradshaw, P.
1964.
Wind-Tunnel Screens: Flow Instability and its Effect on Aerofoil Boundary Layers.
The Journal of the Royal Aeronautical Society,
Vol. 68,
Issue. 639,
p.
198.
Kruka, V.
and
Eskinazi, S.
1964.
The wall-jet in a moving stream.
Journal of Fluid Mechanics,
Vol. 20,
Issue. 4,
p.
555.
SIGALLA, ARMAND
1965.
Calibration of preston tubes in supersonic flow.
AIAA Journal,
Vol. 3,
Issue. 8,
p.
1531.
XERIKOS, J.
and
ANDERSON, W. A.
1965.
Blunt-body integral method for air in thermodynamic equilibrium.
AIAA Journal,
Vol. 3,
Issue. 8,
p.
1531.
Patel, V. C.
1965.
Calibration of the Preston tube and limitations on its use in pressure gradients.
Journal of Fluid Mechanics,
Vol. 23,
Issue. 01,
p.
185.
Bradshaw, P.
1965.
The effect of wind-tunnel screens on nominally two-dimensional boundary layers.
Journal of Fluid Mechanics,
Vol. 22,
Issue. 04,
p.
679.
Patel, Rajni P.
1966.
A note on Turbulent Skin Friction measured with a Preston Tube.
The Journal of the Royal Aeronautical Society,
Vol. 70,
Issue. 671,
p.
1043.
Duffy, J.
and
Norbury, J. F.
1967.
The Static Hole Pair as a Skin Friction Meter.
The Journal of the Royal Aeronautical Society,
Vol. 71,
Issue. 673,
p.
55.
Bradshaw, P.
and
Galea, P. V.
1967.
Step-induced separation of a turbulent boundary layer in incompressible flow.
Journal of Fluid Mechanics,
Vol. 27,
Issue. 1,
p.
111.
Bradshaw, P.
1967.
The turbulence structure of equilibrium boundary layers.
Journal of Fluid Mechanics,
Vol. 29,
Issue. 4,
p.
625.
Duffy, J.
and
Norbury, J. F.
1967.
Paper 7: The Measurement of Skin Friction in Pressure Gradients Using a Static Hole Pair.
Proceedings of the Institution of Mechanical Engineers, Conference Proceedings,
Vol. 182,
Issue. 8,
p.
76.
RAJARATNAM, N.
1967.
Vol. 4,
Issue. ,
p.
197.
Good, M. C.
and
Joubert, P. N.
1968.
The form drag of two-dimensional bluff-plates immersed in turbulent boundary layers.
Journal of Fluid Mechanics,
Vol. 31,
Issue. 3,
p.
547.
SIMPSON, ROGER L.
and
WHITTEN, DERRILL G.
1968.
Preston tubes in the transpired turbulent boundary layer..
AIAA Journal,
Vol. 6,
Issue. 9,
p.
1776.
Aldridge, Keith D.
and
Toomre, Alar
1969.
Axisymmetric inertial oscillations of a fluid in a rotating spherical container.
Journal of Fluid Mechanics,
Vol. 37,
Issue. 2,
p.
307.
Mair, W. A.
1969.
Reduction of Base Drag by Boat-Tailed Afterbodies in Low-Speed Flow.
Aeronautical Quarterly,
Vol. 20,
Issue. 4,
p.
307.
Brown, K. C.
and
Joubert, P. N.
1969.
The measurement of skin friction in turbulent boundary layers with adverse pressure gradients.
Journal of Fluid Mechanics,
Vol. 35,
Issue. 4,
p.
737.
Head, M. R.
and
Ram, V. Vasanta
1971.
Simplified Presentation of Preston Tube Calibration.
Aeronautical Quarterly,
Vol. 22,
Issue. 3,
p.
295.
Duffy, J.
and
Cain, D.
1972.
On the use of the Preston tube in elliptical ducts.
The Aeronautical Journal ,
Vol. 76,
Issue. 738,
p.
371.
Antonia, R. A.
and
Luxton, R. E.
1972.
The response of a turbulent boundary layer to a step change in surface roughness. Part 2. Rough-to-smooth.
Journal of Fluid Mechanics,
Vol. 53,
Issue. 4,
p.
737.