Transition and Stability of High-Speed Boundary Layers

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Brès GA, Inkman M, Colonius T, Fedorov AV. 2009. Alternate designs of ultrasonic absorptive coatings for hypersonic boundary layer control. Presented at AIAA Fluid Dyn. Conf., 39th, San Antonio, AIAA Pap. 2009-4217

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Fedorov AV. 2003a. Receptivity of high-speed boundary layer to acoustic disturbances. J. Fluid Mech. 491:101–29

Fedorov AV. 2003b. Receptivity of hypersonic boundary layer to acoustic disturbances scattered by surface roughness. Presented at AIAA Fluid Dyn. Conf. Exhib., 33rd, Orlando, AIAA Pap. 2003-3731

Fedorov AV. 2010. Temporal stability of hypersonic boundary layer on porous wall: comparison of theory with DNS. Presented at AIAA Aerosp. Sci. Meet., 48th, Orlando, AIAA Pap. 2010-1242

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Fedorov AV, Khokhlov AP. 1993. Excitation and evolution of unstable disturbances in supersonic boundary layer. Proc. ASME Fluid Eng. Conf. 151:1–13

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Fedorov AV, Khokhlov AP. 2002. Receptivity of hypersonic boundary layer to wall disturbances. Theoret. Comput. Fluid Dyn. 15:231–54

Fedorov AV, Kozlov VF, Shiplyuk AN, Maslov AA, Sidorenko AA, et al. 2003a. Stability of hypersonic boundary layer on porous wall with regular microstructure. Presented at AIAA Fluid Dyn. Conf. Exhib., 33rd, Orlando, AIAA Pap. 2003-4147

Fedorov AV, Malmuth ND, Rasheed A, Hornung HG. 2001. Stabilization of hypersonic boundary layers by porous coatings. AIAA J. 39(4):605–10

Fedorov AV, Shiplyuk AN, Maslov AA, Burov EV, Malmuth ND. 2003b. Stabilization of a hypersonic boundary layer using an ultrasonically absorptive coating. J. Fluid Mech. 479:99–124

Fedorov AV, Tumin AM. 2003. Initial-value problem for hypersonic boundary-layer flows. AIAA J. 41(3):379–89

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Johnson HB, Alba CR, Candler GV. 2008. Boundary-layer stability analysis of the hypersonic international flight research transition experiments. J. Spacecr. Rockets 45(2):228–36

Johnson HB, Candler GV. 2005. Hypersonic boundary layer stability analysis using PSE-chem. Presented at AIAA Fluid Dyn. Conf. Exhib., 35th, Toronto, AIAA Pap. 2005-5023

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Kimmel R. 2003. Aspects of hypersonic boundary layer transition control. Presented at Aerosp. Sci. Meet. Exhib., 41st, Reno, AIAA Pap. 2003-772

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Leyva IA, Stuart L, Beierholm A, Hornung HG, Wagnild R, Candler G. 2009. Transition delay in hypervelocity boundary layers by means of CO2/acoustic instability interactions. Presented at AIAA Aerosp. Sci. Meet., 47th, Minneapolis, AIAA Pap. 2009-1287

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Mack LM. 1975a. A numerical method for the prediction of high speed boundary-layer transition using linear theory. NASA SP-347, pp. 101–23, Langley Res. Center

Mack LM. 1975b. Linear stability theory and the problem of supersonic boundary-layer transition. AIAA J. 13(3):278–89

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Mack LM. 1984. Boundary-layer linear stability theory. AGARD Rep. 709, Spec. Course Stab. Transit. Laminar Flows Provides an excellent introduction to linear stability theory for compressible boundary-layer flows.

Malik MB. 1989. Prediction and control of transition in supersonic and hypersonic boundary layers. AIAA J. 27(11):1487–93

Malik MB. 1997. Boundary-layer transition prediction toolkit. Presented at AIAA Fluid Dyn. Conf., 28th, Snowmass Village, CO, AIAA Pap. 1997-1904

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Maslov AA, Shiplyuk AA, Sidorenko AA, Arnal D. 2001. Leading edge receptivity of a hypersonic boundary layer on a flat plate. J. Fluid Mech. 426:73–79 Presents unique experimental data on the leading-edge receptivity of hypersonic boundary layers.

Maslov A, Shiplyuk A, Sidorenko A, Polivanov P, Fedorov A, et al. 2006. Hypersonic laminar flow control using a porous coating of random microstructure. Presented at AIAA Aerosp. Sci. Meet. Exhib., 44th, Reno, AIAA Pap. 2006-1112

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Rasheed A, Hornung HG, Fedorov AV, Malmuth ND. 2002. Experiments on passive hypervelocity boundary layer control using an ultrasonically absorptive surface. AIAA J. 40(3):481–89 Presents first experimental demonstration of hypersonic laminar flow control using porous coatings.

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Reshotko E. 1991. Hypersonic stability and transition. In Hypersonic Flows for Reentry Problems, Vol. 1, ed. JA Desideri, R Glowinski, J Periaux, pp. 18–34. Springer: Berlin

Reshotko E. 2006. Transition issues at hypersonic speeds. Presented at AIAA Aerosp. Sci. Meet. Exhib., 44th, Reno, AIAA Pap. 2006-707

Reshotko E. 2008. Transition issues for atmospheric entry. J. Spacecr. Rockets 45(2):161–64

Sandham ND, Lüdeke H. 2009. Numerical study of Mach 6 boundary-layer stabilization by means of a porous surface. AIAA J. 47(9):2243–52

Saric WS, Reshotko E, Arnal D. 1998. Hypersonic laminar-turbulent transition. AGARD AR-391, Vol. 2, Hypersonic Experimental and Computational Capability, Improvement and Validation Provides an excellent overview of transition problems with emphasis on their modeling.

Schmid PJ, Henningson DS. 2001. Stability and Transition in Shear Flows. New York: Springer-Verlag

Schmisseur JD, Schneider SP. 1998. Receptivity of the Mach-4 boundary layer on an elliptic cone to laser-generated localized free-stream perturbations. Presented at AIAA Aerosp. Sci. Meet. Exhib., 37th, Reno, AIAA Pap. 1998-0532

Schneider SP. 1999. Flight data for boundary layer transition at hypersonic and supersonic speeds. J. Spacecr. Rockets 36(1):8–20 Presents the most comprehensive set of flight data on transition of high-speed boundary-layer flows.

Schneider SP. 2004. Hypersonic laminar-turbulent transition on circular cones and scramjet forebodies. Prog. Aerosp. Sci. 40(1):1–50

Schneider SP. 2006. Laminar-turbulent transition on reentry capsules and planetary probes. J. Spacecr. Rockets 43(6):1153–73

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Stetson KF, Kimmel RL. 1992. On hypersonic boundary-layer stability. Presented at AIAA Aerosp. Sci. Meet. Exhib., 30th, Reno, AIAA Pap. 1992-0737 Presents a detailed discussion of wind-tunnel stability measurements and related physical mechanisms.

Stetson KF, Kimmel RL, Thompson ER, Donaldson JC, Siler LG. 1991. A comparison of planar and conical boundary layer stability and transition at a Mach number of 8. Presented at AIAA Fluid Dyn. Plasma Dyn. Lasers Conf., 22nd, Honolulu, AIAA Pap. 1991-1639

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Tumin A, Wang X, Zhong X. 2007. Direct numerical simulation and the theory of receptivity in a hypersonic boundary. Phys. Fluids 19(1):1–14

Wagnild RM, Candler GV, Leyva IA, Jewell JS, Hornung HG. 2010. Carbon dioxide injection for hypervelocity boundary layer stability. Presented at AIAA Aerosp. Sci. Meet., 48th, Orlando, AIAA Pap. 2010-1244

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Zhigulev VN, Tumin AM. 1987. Onset of Turbulence. Novosibirsk: Nauka Thoroughly discusses theoretical aspects of receptivity and stability of boundary-layer flows.