Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by
Crossref.
Cooke, J. C.
1962.
Boundary-Layer Flow Between the Attachment Lines on a Flat Plate Delta Wing at Incidence.
Aeronautical Quarterly,
Vol. 13,
Issue. 1,
p.
1.
Gaster, M.
1967.
On the Flow Along Swept Leading Edges.
Aeronautical Quarterly,
Vol. 18,
Issue. 2,
p.
165.
Pfenninger, W.
1968.
FLOW PROBLEMS OF SWEPT LOW‐DRAG SUCTION WINGS OF PRACTICAL CONSTRUCTION AT HIGH REYNOLDS NUMBERS*.
Annals of the New York Academy of Sciences,
Vol. 154,
Issue. 2,
p.
672.
Poll, D.I.A.
1983.
The Development of Intermittent Turbulence on a Swept Attachment Line Including the Effects of Compressibility.
Aeronautical Quarterly,
Vol. 34,
Issue. 1,
p.
1.
Narasimha, R.
1985.
The laminar-turbulent transition zone in the boundary layer.
Progress in Aerospace Sciences,
Vol. 22,
Issue. 1,
p.
29.
Pfenninger, Werner
and
Vemuru, Chandra S.
1988.
Design Aspects of Long Range Supersonic LFC Airplanes with Highly Swept Wings.
Vol. 1,
Issue. ,
Kimmel, R. L.
1997.
The Effect of Pressure Gradients on Transition Zone Length in Hypersonic Boundary Layers.
Journal of Fluids Engineering,
Vol. 119,
Issue. 1,
p.
36.
Flynn, G.
and
Jones, R.
1999.
Attachment line transition with 3D isolated roughness elements.
GUÉGAN, ALAN
SCHMID, PETER J.
and
HUERRE, PATRICK
2008.
Spatial optimal disturbances in swept attachment-line boundary layers.
Journal of Fluid Mechanics,
Vol. 603,
Issue. ,
p.
179.