Separation and Transition on a Cone-Cylinder-Flare: Experimental Campaigns-Reference-Cited by-同舟云学术

Separation and Transition on a Cone-Cylinder-Flare: Experimental Campaigns

Published:2024-01-04 Issue: Volume: Page:
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Container-title:AIAA SCITECH 2024 Forum
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Author:

Benitez Elizabeth K.¹,Borg Matthew P.¹,Esquieu Sébastien²,Caillaud Clément²,Lugrin Mathieu³,McDaniel Zachary A.⁴,Jewell Joseph S.⁴,Scholten Anton⁵,Paredes Pedro⁶,Li Fei⁷,Choudhari Meelan M.⁷

Affiliation:

1. Air Force Research Laboratory

2. Commissariat a l'energie atomique et aux energies alternatives Siege administratif

3. ONERA Mecanique des fluides et energetique

4. Purdue University

5. NC State University

6. National Institute of Aerospace

7. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2024-0496

Reference35 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. Input-Output Analysis of Shock Boundary Layer Interaction

4. Boundary Layer Transition on a Generic Model of Control Flaps in Hypersonic Flow

5. Transition scenario in hypersonic axisymmetrical compression ramp flow

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