Influence of roughness on attachment line boundary layer transition in hypersonic flow

Experiments in Fluids

Volumn 22, Issue 4, 1997, Pages 286-291

  Benard, E ^a   Gaillard, L ^a   Alziary De Roquefort, T ^a  

^a CEAT   (France)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0001248681     PISSN: 07234864     EISSN: None     Source Type: Journal    
DOI: 10.1007/s003480050050     Document Type: Article

References (16)

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2. Beckwith IE (1958) Similar solutions for the compressible boundary layer on a yawed cylinder with transpiration cooling. NACA TN 4345
3. Bushnell DM; Huffmann JK (1967) Investigation of heat transfer to leading edge of a 76° swept fin with and without chordwise slots and correlations of swept leading edge transition data for Mach 2 to 8. NASA TMX 1475
4. Creel TR Jr; Beckwith IE; Chen FJ (1987) Transition on swept leading edges at Mach 3.5. J. Aircraft 25: 710-717
5. Da Costa JL (1990) Contribution à l'étude de transition de bord d'attaque par contamination en écoulement hypersonique. Ph.D. Thesis, University of Poitiers, France
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7. Gaster M (1967) On the flow along swept leading edges. Aero Quat 18: 165-184
8. Holden MS; Kolly JM (1995) Attachment line transition studies on swept cylindrical leading edges at Mach numbers from 10 to 12. AIAA Paper 95-2279
9. Morkovin MV (1969) On the many faces of transition. In: Viscous Drag Reduction, 1-31, C.S. Wells, Ed.. Plenum Press New York
10. Morkovin MV (1990) On roughness-induced transition: facts, views, and speculations. In: Instability and Transition, Vol. 1, 281-295, M.Y. Hussaini, R.G. Voigt, Ed., Springer Berlin
11. Murakami A; Stanewsky E; Krogmann P (1996) Boundary-layer transition on swept cylinders at hypersonic speeds. AIAA J 34: 649-654
12. Poll DIA (1979) Transition in the infinite swept attachment line boundary layer. Aero Quat 30: 607-629
13. Poll DIA (1981) Skin friction and heat transfer at an infinite swept attachment line. Aero Quat 32: 299-318
14. Poll DIA (1990) The effect of isolated roughness elements on transition in attachment-line flows. D. Arnal, R. Michel (Eds) Laminar-Turbulent Transition IUTAM Symposium Toulouse/ France 1989, pp. 657-667, Springer Berlin
15. Skuratov AS; Fedorov AV (1991) Supersonic boundary layer transition induced by roughness on the attachment of a yawed cylinder. Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, no 6: 28-35. Moscow
16. Wurster KE (1981) An assessment of the impact of transition on advanced protection system mass. AIAA Paper 81-1090