Measurement of Hypersonic Boundary Layer Transition on Cone Models in the Free-Piston Shock Tunnel HIEST-Reference-Cited by-同舟云学术

Measurement of Hypersonic Boundary Layer Transition on Cone Models in the Free-Piston Shock Tunnel HIEST

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
language:
Short-container-title:

Author:

Tanno Hideyuki¹,Komuro Tomoyuki¹,Sato Kazuo¹,Itoh Katsuhiro¹,Takahashi Masahiro¹,Fujii Keisuke¹

Affiliation:

1. Japan Aerospace Exploration Agency

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-781

Reference8 articles.

1. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies

2. Experiment of the Two-Dimensional Roughness Effect on Hypersonic Boundary-Layer Transition

3. Hypersonic aerothermodynamic and scramjet research using high enthalpy shock tunnel

4. 5Wadhams, T.P., E. Mundy, E., MacLean, M.G. and Holden, M.S. "Pre-Flight Ground Testing of the Full-Scale HFiRE-1 VehicleatFullyDuplicatedFlightConditions:PartII",AIAAPaperNo.2008-0639,2008.

Cited by 27 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. Time-resolved wave packet development in highly cooled hypersonic boundary layers;Journal of Fluid Mechanics;2024-03-21

2. High Enthalpy Effects on Hypersonic Boundary-Layer Transition: T5 Experimental and Numerical Comparison;AIAA SCITECH 2024 Forum;2024-01-04

3. Hypersonic Boundary-Layer Disturbances on a Cooled, Slender Cone at Mach 6;Journal of Spacecraft and Rockets;2023-03

4. Enthalpy Effects on Disturbance Growth in high-enthalpy hypersonic flow;AIAA SCITECH 2023 Forum;2023-01-19

5. Boundary-Layer Disturbances and Surface Heat-Flux Profiles on a Cooled Slender Cone;AIAA SCITECH 2022 Forum;2022-01-03