论文信息 - Performance Improvements in Boeing/AFOSR Mach 6 Quiet Wind Tunnel Based on CFD Predictions

Performance Improvements in Boeing/AFOSR Mach 6 Quiet Wind Tunnel Based on CFD Predictions

Abstract : MOTIVATION: Importance of quiet tunnels for hypersonic research -- Understanding the nature of laminar-to-turbulent transition is crucial for: * Reusable launch vehicles * Hypersonic reconnaissance aircraft * Hypersonic cruise vehicles * Ballistic reentry vehicles * Current Programs * DARPA FALCON glide vehicle * X-51 * Orion

[1] J. Hess,et al. Calculation of potential flow about arbitrary bodies , 1967 .

[2] Steven P. Schneider. Laminar-Turbulent Transition on Reentry Capsules and Planetary Probes , 2006 .

[3] S. Aradag,et al. Bleed Lip Geometry Effects on the Flow in a Hypersonic Wind Tunnel , 2006 .

[4] I. E. Beckwith,et al. Design requirements for the NASA Langley supersonic low-disturbance wind tunnel , 1986 .

[5] Steven P. Schneider,et al. Development of Hypersonic Quiet Tunnels , 2008 .

[6] Dan S. Henningson,et al. A numerical and experimental study of a transitional separation bubble , 2001 .

[7] Shann J. Rufer,et al. Hypersonic Transition Research in the Boeing/AFOSR Mach-6 Quiet Tunnel , 2003 .

[8] D. Wilcox. Turbulence modeling for CFD , 1993 .

[9] Thomas J. Juliano,et al. High-Reynolds-Number Laminar Flow in the Mach-6 Quiet-Flow Ludwieg Tube , 2006 .

[10] P S Klebanoff,et al. MECHANISM BY WHICH A TWO-DIMENSIONAL ROUGHNESS ELEMENT INDUCES BOUNDARY-LAYER TRANSITION: ROUGHNESS INDUCED TRANSITION , 1972 .

[11] Steven P. Schneider,et al. Computational design of the boeing/AFOSR mach 6 wind tunnel , 2006 .

[12] R. Kimmel,et al. Drag Prediction and Transition in Hypersonic Flow , 1997 .

[13] Craig Ryan Skoch. Disturbances from shock/boundary-layer interactions affecting upstream hypersonic flow , 2005 .