Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by
Crossref.
POLL, D.
1985.
Boundary layer transition on the windward face of Space Shuttle during re-entry.
Poll, D. I. A.
1986.
A new hypothesis for transition on the windward face of the Space Shuttle.
Journal of Spacecraft and Rockets,
Vol. 23,
Issue. 6,
p.
605.
HOLDEN, M.
1986.
A review of aerothermal problems associated with hypersonic flight.
Creel, T. R.
Malik, M. R.
and
Beckwith, I. E.
1987.
Boundary-Layer Instability Mechanisms on a Swept-Leading Edge at Mach 3.5.
Vol. 1,
Issue. ,
Creel, T. R.
Beckwith, I. E.
and
Chen, F. J.
1987.
Transition on swept leading edges at Mach 3.5.
Journal of Aircraft,
Vol. 24,
Issue. 10,
p.
710.
Ahmed, Anwar
Wentz, William H.
and
Nyenhuis, R.
1989.
In-flight boundary-layer transition measurements on a swept wing.
Journal of Aircraft,
Vol. 26,
Issue. 11,
p.
979.
Arnal, D.
Vignau, F.
and
Juillen, J. C.
1990.
Laminar-Turbulent Transition.
p.
669.
CREEL, T.
1991.
Effects of sweep angle and passive relaminarization devices on a supersonic swept-cylinder boundary layer.
Kazakov, A. V.
1991.
Effect of surface temperature on the stability of the swept attachment line boundary layer.
Fluid Dynamics,
Vol. 25,
Issue. 6,
p.
875.
Skuratov, A. S.
and
Fedorov, A. V.
1992.
Supersonic boundary layer transition induced by roughness on the attachment line of a yawed cylinder.
Fluid Dynamics,
Vol. 26,
Issue. 6,
p.
816.
Stollery, J. L.
1992.
Hypersonic Flows for Reentry Problems.
p.
68.
Theofilis, Vassilios
1993.
Numerical experiments on the stability of leading edge boundary layer flow: A two‐dimensional linear study.
International Journal for Numerical Methods in Fluids,
Vol. 16,
Issue. 2,
p.
153.
Theofilis, V.
1994.
The discrete temporal eigenvalue spectrum of the generalised Hiemenz flow as solution of the Orr-Sommerfeld equation.
Journal of Engineering Mathematics,
Vol. 28,
Issue. 3,
p.
241.
Lin, R.-S.
and
Malik, M. R.
1995.
Stability and Transition in Compressible Attachment-Line Boundary-Layer Flow.
Vol. 1,
Issue. ,
Holden, Michael
and
Kolly, Joseph
1995.
Attachment line transition studies on swept cylindrical leading edges at Mach numbers from 10 to 12.
Coleman, Colin
Laub, James
Poll, D.
and
Wolf, Stephen
1996.
Leading edge transition on a 76 degree swept cylinder at Mach 1.6.
Kazakov, A. V.
1998.
Effect of Heat Supply on the Stability of the Supersonic Swept Atiachment-Line Boundary Layer.
Fluid Dynamics,
Vol. 33,
Issue. 5,
p.
710.
Lin, Ray-Sing
and
Malik, Mujeeb
1999.
Oblique modes in attachment-line boundary layer.
Flynn, G.
and
Jones, R.
1999.
Attachment line transition with 3D isolated roughness elements.
Dietz, Anthony
Coleman, Colin
Laub, Jim
and
Poll, D. I. A.
2000.
Laminar-Turbulent Transition.
p.
249.