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Title: Hypersonic Fluid-Structure Interactions on a Slender Cone

Journal Article · · AIAA Journal
DOI:https://doi.org/10.2514/6.2018-1825· OSTI ID:1477865
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  1. Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
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Fluid-structure interactions were studies on a 7° half-angle cone in the Sandia Hypersonic Wind Tunnel at Mach 5 and 8 and in the Purdue Boeing/AFOSR Mach 6 Quiet Tunnel. A thin composite panel was integrated into the cone and the response to boundary-layer disturbances was characterized by accelerometers on the backside of the panel. Here, under quiet-flow conditions at Mach 6, the cone boundary layer remained laminar. Artificially generated turbulent spots excited a directionally dependent panel response which would last much longer than the spot duration.

Research Organization:
Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
Sponsoring Organization:
USDOE National Nuclear Security Administration (NNSA)
Grant/Contract Number:
AC04-94AL85000
OSTI ID:
1477865
Report Number(s):
SAND-2018-3455J; 662006
Journal Information:
AIAA Journal, Vol. 2018; ISSN 0001-1452
Publisher:
AIAACopyright Statement
Country of Publication:
United States
Language:
English

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Figures / Tables (14)

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Figure 12(p. 14)figure Figure 12

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