Interaction Between Compliant Structures and Boundary-Layer Transition in Hypersonic Flow
暂无分享,去创建一个
[1] Bryan Glaz,et al. Approximate Modeling of Unsteady Aerodynamics for Hypersonic Aeroelasticity , 2010 .
[2] S. Lele,et al. Breakdown mechanisms and heat transfer overshoot in hypersonic zero pressure gradient boundary layers , 2013, Journal of Fluid Mechanics.
[3] J. Halton. On the efficiency of certain quasi-random sequences of points in evaluating multi-dimensional integrals , 1960 .
[4] K. Fujii. Experiment of the Two-Dimensional Roughness Effect on Hypersonic Boundary-Layer Transition , 2006 .
[5] Steven P. Schneider,et al. Hypersonic Boundary-Layer Transition Experiments in the Boeing/AFOSR Mach-6 Quiet Tunnel , 2012 .
[6] Jack J. McNamara,et al. Assessing Hypersonic Boundary-Layer Stability in the Presence of Structural Deformation , 2014 .
[7] Seung-O Park,et al. Study on Stabilization and Destabilization Effect of a Smooth Hump in Hypersonic Boundary Layers by PSE , 2013 .
[8] X. Zhong,et al. Numerical simulation of roughness effect on the stability of a hypersonic boundary layer , 2014 .
[9] Steven P. Schneider,et al. Laminar Boundary-Layer Instabilities on Hypersonic Cones: Computations for Benchmark Experiments , 2005 .
[10] A. Fedorov,et al. Receptivity of Hypersonic Boundary Layer to Wall Disturbances , 2002 .
[11] Steven P. Schneider,et al. Developing mechanism-based methods for estimating hypersonic boundary-layer transition in flight: The role of quiet tunnels , 2013 .
[12] Scott A. Berry,et al. X-33 Hypersonic Boundary Layer Transition , 1999 .
[13] Fei Li,et al. Transition Analysis for the Ascent Phase of HIFiRE-1 Flight Experiment , 2015 .
[14] L. Mack,et al. Transition prediction and linear stability theory , 1977 .
[15] Thomas J. Juliano,et al. Instability and transition measurements in the Mach-6 quiet tunnel , 2009 .
[16] Mark Drela,et al. Implicit Implementation of the Full e^n Transition Criterion , 2003 .
[17] Dean Kontinos,et al. Numerical Simulation of Metallic Thermal Protection System Panel Bowing , 1999 .
[18] Timothy Wadhams,et al. Ground Test Studies of the HIFiRE-1 Transition Experiment Part 2: Computational Analysis , 2008 .
[19] Brent A. Miller,et al. Loosely Coupled Time Integration of Fluid- Thermal-Structural Interactions in Hypersonic Flows , 2015 .
[20] J. D. Crouch,et al. Variable N-Factor Method for Transition Prediction in Three-Dimensional Boundary Layers , 2000 .
[21] M. J. Lighthill,et al. Oscillating Airfoils at High Mach Number , 1953 .
[22] Jack J. McNamara,et al. Time-Marching Considerations for Response Prediction of Structures in Hypersonic Flows , 2015 .
[23] X. Zhong,et al. Second Mode Suppression in Hypersonic Boundary Layer by Roughness: Design and Experiments , 2015 .
[24] Scott A. Berry,et al. Boundary Layer Transition on Slender Cones in Conventional and Low Disturbance Mach 6 Wind Tunnels , 2002 .
[25] S. Schneider. Effects of Roughness on Hypersonic Boundary-Layer Transition , 2007 .
[26] X. Zhong,et al. Receptivity of a Hypersonic Flat-Plate Boundary Layer to Three-Dimensional Surface Roughness , 2008 .
[27] L. R. Hunt,et al. Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5 , 1986 .
[28] Andrew R. Crowell,et al. Robust and Efficient Treatment of Temperature Feedback in Fluid–Thermal–Structural Analysis , 2014 .
[29] Roger L. Kimmel,et al. HIFiRE-1 Boundary-Layer Transition: Ground Test Results and Stability Analysis , 2015 .
[30] I. W. M. Crouch,et al. Transition Prediction for Three-Dimensional Boundary Layers in Computational Fluid Dynamics Applications , 2002 .
[31] Jack J. McNamara,et al. The impact of flow induced loads on snap-through behavior of acoustically excited, thermally buckled panels , 2011 .
[32] S. Berry,et al. Discrete Roughness Transition for Hypersonic Flight Vehicles , 2007 .
[33] Roddam Narasimha,et al. Some properties of boundary layer flow during the transition from laminar to turbulent motion , 1958, Journal of Fluid Mechanics.
[34] G. Iaccarino,et al. Disturbance evolution in a Mach 4.8 boundary layer with two-dimensional roughness-induced separation and shock , 2010, Journal of Fluid Mechanics.
[35] G. Candler,et al. Data-Parallel Line Relaxation Method for the Navier -Stokes Equations , 1998 .
[36] Jack J. McNamara,et al. Studies on Fluid-Thermal-Structural Coupling for Aerothermoelasticity in Hypersonic Flow , 2010 .
[37] Holt Ashley,et al. Piston Theory-A New Aerodynamic Tool for the Aeroelastician , 1956 .
[38] Peretz P. Friedmann,et al. Hypersonic Aeroelastic and Aerothermoelastic Studies Using Computational Fluid Dynamics , 2014 .
[39] Zachary B. Riley,et al. Characterization of Structural Response to Hypersonic Boundary-Layer Transition , 2016 .
[40] Andy J. Keane,et al. Engineering Design via Surrogate Modelling - A Practical Guide , 2008 .
[41] G. Candler,et al. Hypersonic Boundary Layer Stability Analysis Using PSE-Chem , 2005 .
[42] A. Fedorov,et al. Stabilization of a hypersonic boundary layer using a wavy surface , 2013 .