Analysis of Second-Mode Amplitudes on Sharp Cones in Hypersonic Wind Tunnels-Reference-Cited by-同舟云学术

Analysis of Second-Mode Amplitudes on Sharp Cones in Hypersonic Wind Tunnels

Published:2019-03 Issue:2 Volume:56 Page:307-318
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Marineau Eric C.¹,Grossir Guillaume²,Wagner Alexander³,Leinemann Madlen,Radespiel Rolf,Tanno Hideyuki⁴,Chynoweth Brandon C.,Schneider Steven P.,Wagnild Ross M.,Casper Katya M.

Affiliation:

1. Arnold Engineering Development Center, Silver Spring, Maryland 20903

2. von Karman Institute for Fluid Dynamics, 1640 Rhode-St-Genèse, Belgium

3. DLR, German Aerospace Center, Göttingen, Germany 37037

4. Japan Aerospace Exploration Agency, Kakuda 9811525, Japan

Funder

U. S. Dept. of Energy National Nuclear Security Administration

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A34286

Reference44 articles.

1. Surface-Pressure Measurements of Second-Mode Instability in Quiet Hypersonic Flow

2. Measurements and Computations of Second-Mode Instability Waves in Several Hypersonic Wind Tunnels

3. Experimental Study of Second-Mode Instabilities on a 7-Degree Cone at Mach 6

4. Hypersonic Boundary Layer Transition on a 7 Degree Half-Angle Cone at Mach 10

5. Mach 10 Boundary Layer Transition Experiments on Sharp and Blunted Cones (Invited)

Cited by 37 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Breakdown mechanisms induced by stationary crossflow vortices in hypersonic three-dimensional boundary layers;Physics of Fluids;2024-07-01

2. Relaminarization effects in hypersonic flow on a three-dimensional expansion–compression geometry;Journal of Fluid Mechanics;2024-04-22

3. Global analysis of nonlinear second-mode development in a Mach-6 boundary layer from high-speed schlieren data;Experiments in Fluids;2024-01-31

4. Experimental investigation of boundary layer instabilities and transition on sharp and blunt cones in Oxford’s High-Density Tunnel;AIAA SCITECH 2024 Forum;2024-01-04

5. Enhancements to Linear Stability Solver-Based CFD-integrated Transition Prediction for High-Speed Flows;AIAA SCITECH 2024 Forum;2024-01-04