Experimental Measurements of Hypersonic Instabilities over Ogive-Cylinders at Mach 6-Reference-Cited by-同舟云学术

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Experimental Measurements of Hypersonic Instabilities over Ogive-Cylinders at Mach 6

Published:2022-08 Issue:8 Volume:60 Page:4492-4508
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Hill J. Luke¹^ORCID,Oddo Ryan A.¹,Komives Jeffrey R.¹,Reeder Mark F.¹,Borg Matthew P.²,Jewell Joseph S.³

Affiliation:

1. Air Force Institute of Technology, Wright–Patterson Air Force Base, Ohio 45433

2. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433

3. Purdue University, West Lafayette, Indiana 47907

Funder

Air Force Research Laboratory, Munitions Directorate

Hypersonic Vehicle Simulation Institute

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J061019

Reference44 articles.

1. BrinichP. F. “Effects of Leading-Edge Geometry on Boundary Layer Transition at Mach 3.1,” NACA TN 3659, 1956.

2. MoeckelW. E. “Some Effects of Bluntness on Boundary Layer Transition and Heat Transfer at Supersonic Speeds,” NACA TN 1312, 1957.

3. MackL. M. “Boundary-Layer Linear Stability Theory,” AGARD Rept. 709, Vol. 3, 1984.

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4. Investigation of Transition Mechanisms in Blunt-tip Ogive-cylinder Forebodies;AIAA SCITECH 2024 Forum;2024-01-04

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