Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by Crossref.
Bradbury, L. J. S.
1965.
The structure of a self-preserving turbulent plane jet.
Journal of Fluid Mechanics,
Vol. 23,
Issue. 01,
p.
31.
Fiedler, H.
and
Head, M. R.
1966.
Intermittency measurements in the turbulent boundary layer.
Journal of Fluid Mechanics,
Vol. 25,
Issue. 4,
p.
719.
Giles, J. A.
Hays, A. P.
and
Sawyer, R. A.
1966.
Turbulent Wall Jets on Logarithmic Spiral Surfaces.
Aeronautical Quarterly,
Vol. 17,
Issue. 3,
p.
201.
Demetriades, Anthony
1968.
Turbulent front structure of an axisymmetric compressible wake.
Journal of Fluid Mechanics,
Vol. 34,
Issue. 3,
p.
465.
DEMETRIADES, A.
and
DOUGHMAN, E.
1968.
Observations in the transition zone of a turbulent plasma jet.
Wygnanski, I.
and
Fiedler, H.
1969.
Some measurements in the self-preserving jet.
Journal of Fluid Mechanics,
Vol. 38,
Issue. 3,
p.
577.
OWEN, F.
1969.
Transition experiments on a flat plate at subsonic and supersonic speeds.
OWEN, F. K.
1970.
Transition experiments on a flat plate at subsonic and supersonic speeds.
AIAA Journal,
Vol. 8,
Issue. 3,
p.
518.
BOLDMAN, DONALD R.
and
NEUMANN, HARVEY E.
1970.
Intermittency in a highly accelerated boundary layer.
AIAA Journal,
Vol. 8,
Issue. 10,
p.
1899.
Kibens, Valdis
Kovasznay, Leslie S. G.
and
Oswald, Lawrence J.
1974.
Turbulent-nonturbulent interface detector.
Review of Scientific Instruments,
Vol. 45,
Issue. 9,
p.
1138.
Blackwelder, Ron F.
1978.
Proceedings of the Dynamic Flow Conference 1978 on Dynamic Measurements in Unsteady Flows.
p.
173.
Wentz, W. H.
Ahmed, A.
and
Nyenhuis, R.
1985.
Further Results of Natural Laminar Flow Flight Test Experiments.
Vol. 1,
Issue. ,
Akhlaghi, H.
Soltani, M.R.
and
Maghrebi, M.J.
2020.
Laminar-turbulent intermittency measurement based on the uncalibrated hot-film data.
Measurement,
Vol. 156,
Issue. ,
p.
107575.
Lai, Yi-Huei
and
Miau, Jiun-Jih
2021.
An investigation into the nonstationary characteristics of separation-bubble formation on a smooth circular cylinder in the critical transition range.
Journal of Mechanics,
Vol. 37,
Issue. ,
p.
415.