Free-stream receptivity of a hypersonic blunt cone using input–output analysis and a shock-kinematic boundary condition-Reference-Cited by-同舟云学术

Free-stream receptivity of a hypersonic blunt cone using input–output analysis and a shock-kinematic boundary condition

Published:2022-01-11 Issue:1 Volume:36 Page:155-180
ISSN:0935-4964
Container-title:Theoretical and Computational Fluid Dynamics
language:en
Short-container-title:Theor. Comput. Fluid Dyn.

Author:

Cook David A.^ORCID,Nichols Joseph W.

Funder

Office of Naval Research

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,General Engineering,Condensed Matter Physics,Computational Mechanics

Link

https://link.springer.com/content/pdf/10.1007/s00162-021-00597-5.pdf

Reference51 articles.

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3. Lin, T.C.: Influence of laminar boundary-layer transition on entry vehicle design. J. Spacecr. Rockets 45(2), 165 (2008)

4. Mack, L.M.: The inviscid stability of the compressible laminar boundary layer. Technical Report, pp. 37–23. Space Programs Summary (1963)

5. Mack, L.M.: Boundary-layer linear stability theory. Technical Report, p. 709, Part 3, AGARD Report (1984)

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