Assessment of Linear Methods for Analysis of Boundary Layer Instabilities on a Finned Cone at Mach 6-Reference-Cited by-同舟云学术

Assessment of Linear Methods for Analysis of Boundary Layer Instabilities on a Finned Cone at Mach 6

Published:2022-06-20 Issue: Volume: Page:
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Container-title:AIAA AVIATION 2022 Forum
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Author:

Araya Daniel¹,Bitter Neal¹,Wheaton Bradley M.¹,Kamal Omar²,Colonius Tim²,Knutson Anthony³,Johnson Heath⁴,Nichols Joseph³,Candler Graham V.³,Russo Vincenzo⁵,Brehm Christoph⁶

Affiliation:

1. Johns Hopkins University Applied Physics Laboratory

2. California Institute of Technology

3. University of Minnesota Twin Cities

4. Virtus Aero, LLC

5. University of Kentucky, University of Kentucky, Lexington, KY, US, academic

6. University of Maryland at College Park

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-3247

Reference81 articles.

1. Mack, L. M. "Boundary-Layer Linear Stability Theory," Tech. Rep. AGARD Report No. 709, Part 3, California Institue of Technology Jet Propulsion Laboratory, 1984.

2. Developing mechanism-based methods for estimating hypersonic boundary-layer transition in flight: The role of quiet tunnels

3. Boundary-Layer Stability Analysis for Stetson’s Mach 6 Blunt-Cone Experiments

4. STABILITY AND TRANSITION OF THREE-DIMENSIONAL BOUNDARY LAYERS

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