Measurements on a Blunt Cone-Cylinder-Flare at Mach 6-Reference-Cited by-同舟云学术

Measurements on a Blunt Cone-Cylinder-Flare at Mach 6

Published:2023-01-19 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2023 Forum
language:
Short-container-title:

Author:

Benitez Elizabeth K.¹,Borg Matthew P.¹,Hill Jonathan L.²,Scholten Anton³,Paredes Pedro⁴,Jewell Joseph S.⁵

Affiliation:

1. Air Force Research Laboratory

2. Air Force Institute of Technology

3. NC State University

4. National Institute of Aerospace

5. Purdue University

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2023-1245

Reference45 articles.

1. Becker, J., and Korycinski, P. "Heat Transfer and Pressure Distribution at a Mach Number of 6.8 on Bodies with Conical Flares and Extensive Flow Separation," Tech. Rep. RM L56F22, NACA,Apr. 1956. DTIC citationAD0274584.

2. Ginoux, J. "Investigation of Flow Separation over Ramps at M∞=3," Tech. Rep. AEDC-TR-65-273, Von Karman Gas Dynamics Facility, Arnold Engineering Development Center, Dec. 1965.

3. Stability of Hypersonic Boundary Layers over a Compression Corner

4. Shock Wave/Transitional Boundary-Layer Interactions in Hypersonic Flow

Cited by 4 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. Nosetip bluntness effects on a cone-cylinder-flare at mach 6;Experiments in Fluids;2024-04-30

2. Separation and Transition on a Cone-Cylinder-Flare: Experimental Campaigns;AIAA SCITECH 2024 Forum;2024-01-04

3. Effect of Angle of Attack on Separation Bubble Instability and Transition on a Cone-Slice-Ramp in Mach-6 Quiet Flow;AIAA SCITECH 2024 Forum;2024-01-04

4. Study of Bluntness-Induced Elongated Structures in Hypersonic Flow over a 7 degree Circular Cone;AIAA SCITECH 2023 Forum;2023-01-19