Sharp-fin induced shock wave/turbulent boundary layer interactions in an axisymmetric configuration

Joshua D. Pickles; Pramod K. Subbareddy; Venkateswaran Narayanaswamy

doi:10.2514/6.2016-3340

Sharp-fin induced shock wave/turbulent boundary layer interactions in an axisymmetric configuration

Joshua D. Pickles
, Pramod K. Subbareddy
, Venkateswaran Narayanaswamy

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

7 Scopus citations

Abstract

Novel data from complimentary experimental and computational studies are presented for shock/boundary layer interactions induced by a sharp fin in an axisymmetric configuration. Fin configurations of 5°, 10°, 12°, 14°, and 20° were tested in a Mach number of 3 while mounted to a half-cylinder with a 100-mm outer diameter. RANS simulations are currently underway using a grid developed for this axisymmetric configuration. Flow visualizations with aluminum oxide show the presence of primary separation, but do not indicate definite existence of primary reattachment or secondary separation/reattachment.

Original language	English (US)
Title of host publication	46th AIAA Fluid Dynamics Conference
Publisher	American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)	9781624104367
DOIs	https://doi.org/10.2514/6.2016-3340
State	Published - 2016
Externally published	Yes
Event	46th AIAA Fluid Dynamics Conference, 2016 - Washington, United States Duration: Jun 13 2016 → Jun 17 2016

Publication series

Name	46th AIAA Fluid Dynamics Conference

Other

Other	46th AIAA Fluid Dynamics Conference, 2016
Country/Territory	United States
City	Washington
Period	6/13/16 → 6/17/16

Bibliographical note

Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

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10.2514/6.2016-3340

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Sharp-fin induced shock wave/turbulent boundary layer interactions in an axisymmetric configuration. / Pickles, Joshua D.; Subbareddy, Pramod K.; Narayanaswamy, Venkateswaran.
46th AIAA Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, 2016. (46th AIAA Fluid Dynamics Conference).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Pickles, JD, Subbareddy, PK & Narayanaswamy, V 2016, Sharp-fin induced shock wave/turbulent boundary layer interactions in an axisymmetric configuration. in 46th AIAA Fluid Dynamics Conference. 46th AIAA Fluid Dynamics Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, 46th AIAA Fluid Dynamics Conference, 2016, Washington, United States, 6/13/16. https://doi.org/10.2514/6.2016-3340

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title = "Sharp-fin induced shock wave/turbulent boundary layer interactions in an axisymmetric configuration",

abstract = "Novel data from complimentary experimental and computational studies are presented for shock/boundary layer interactions induced by a sharp fin in an axisymmetric configuration. Fin configurations of 5°, 10°, 12°, 14°, and 20° were tested in a Mach number of 3 while mounted to a half-cylinder with a 100-mm outer diameter. RANS simulations are currently underway using a grid developed for this axisymmetric configuration. Flow visualizations with aluminum oxide show the presence of primary separation, but do not indicate definite existence of primary reattachment or secondary separation/reattachment.",

author = "Pickles, \{Joshua D.\} and Subbareddy, \{Pramod K.\} and Venkateswaran Narayanaswamy",

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doi = "10.2514/6.2016-3340",

language = "English (US)",

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AU - Pickles, Joshua D.

AU - Subbareddy, Pramod K.

AU - Narayanaswamy, Venkateswaran

PY - 2016

Y1 - 2016

N2 - Novel data from complimentary experimental and computational studies are presented for shock/boundary layer interactions induced by a sharp fin in an axisymmetric configuration. Fin configurations of 5°, 10°, 12°, 14°, and 20° were tested in a Mach number of 3 while mounted to a half-cylinder with a 100-mm outer diameter. RANS simulations are currently underway using a grid developed for this axisymmetric configuration. Flow visualizations with aluminum oxide show the presence of primary separation, but do not indicate definite existence of primary reattachment or secondary separation/reattachment.

AB - Novel data from complimentary experimental and computational studies are presented for shock/boundary layer interactions induced by a sharp fin in an axisymmetric configuration. Fin configurations of 5°, 10°, 12°, 14°, and 20° were tested in a Mach number of 3 while mounted to a half-cylinder with a 100-mm outer diameter. RANS simulations are currently underway using a grid developed for this axisymmetric configuration. Flow visualizations with aluminum oxide show the presence of primary separation, but do not indicate definite existence of primary reattachment or secondary separation/reattachment.

UR - https://www.scopus.com/pages/publications/85088071146

UR - https://www.scopus.com/pages/publications/85088071146#tab=citedBy

U2 - 10.2514/6.2016-3340

DO - 10.2514/6.2016-3340

M3 - Conference contribution

AN - SCOPUS:85088071146

SN - 9781624104367

T3 - 46th AIAA Fluid Dynamics Conference

BT - 46th AIAA Fluid Dynamics Conference

PB - American Institute of Aeronautics and Astronautics Inc, AIAA

T2 - 46th AIAA Fluid Dynamics Conference, 2016

Y2 - 13 June 2016 through 17 June 2016

ER -

Sharp-fin induced shock wave/turbulent boundary layer interactions in an axisymmetric configuration

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