Characterization of structural response to hypersonic boundary-layer transition
Abstract
The inherent relationship between boundary-layer stability, aerodynamic heating, and surface conditions makes the potential for interaction between the structural response and boundary-layer transition an important and challenging area of study in high-speed flows. This paper phenomenologically explores this interaction using a fundamental two-dimensional aerothermoelastic model under the assumption of an aluminum panel with simple supports. Specifically, an existing model is extended to examine the impact of transition onset location, transition length, and transitional overshoot in heat flux and fluctuating pressure on the structural response of surface panels. Transitional flow conditions are found to yield significantly increased thermal gradients, and they can result in higher maximum panel temperatures compared to turbulent flow. Results indicate that overshoot in heat flux and fluctuating pressure reduces the flutter onset time and increases the strain energy accumulated in the panel. Furthermore, overshoot occurring near the midchord can yield average temperatures and peak displacements exceeding those experienced by the panel subject to turbulent flow. Lastly, these results suggest that fully turbulent flow does not always conservatively predict the thermo-structural response of surface panels.
- Authors:
-
- The Ohio State Univ., Columbus, OH (United States)
- Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
- Publication Date:
- Research Org.:
- Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
- Sponsoring Org.:
- USDOE National Nuclear Security Administration (NNSA)
- OSTI Identifier:
- 1259865
- Report Number(s):
- SAND-2015-5512J
Journal ID: ISSN 0001-1452; 594845
- Grant/Contract Number:
- AC04-94AL85000
- Resource Type:
- Accepted Manuscript
- Journal Name:
- AIAA Journal
- Additional Journal Information:
- Journal Name: AIAA Journal; Journal ID: ISSN 0001-1452
- Publisher:
- AIAA
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 42 ENGINEERING
Citation Formats
Riley, Zachary B., Deshmukh, Rohit, Miller, Brent A., McNamara, Jack J., and Casper, Katya M. Characterization of structural response to hypersonic boundary-layer transition. United States: N. p., 2016.
Web. doi:10.2514/1.j054607.
Riley, Zachary B., Deshmukh, Rohit, Miller, Brent A., McNamara, Jack J., & Casper, Katya M. Characterization of structural response to hypersonic boundary-layer transition. United States. https://doi.org/10.2514/1.j054607
Riley, Zachary B., Deshmukh, Rohit, Miller, Brent A., McNamara, Jack J., and Casper, Katya M. Tue .
"Characterization of structural response to hypersonic boundary-layer transition". United States. https://doi.org/10.2514/1.j054607. https://www.osti.gov/servlets/purl/1259865.
@article{osti_1259865,
title = {Characterization of structural response to hypersonic boundary-layer transition},
author = {Riley, Zachary B. and Deshmukh, Rohit and Miller, Brent A. and McNamara, Jack J. and Casper, Katya M.},
abstractNote = {The inherent relationship between boundary-layer stability, aerodynamic heating, and surface conditions makes the potential for interaction between the structural response and boundary-layer transition an important and challenging area of study in high-speed flows. This paper phenomenologically explores this interaction using a fundamental two-dimensional aerothermoelastic model under the assumption of an aluminum panel with simple supports. Specifically, an existing model is extended to examine the impact of transition onset location, transition length, and transitional overshoot in heat flux and fluctuating pressure on the structural response of surface panels. Transitional flow conditions are found to yield significantly increased thermal gradients, and they can result in higher maximum panel temperatures compared to turbulent flow. Results indicate that overshoot in heat flux and fluctuating pressure reduces the flutter onset time and increases the strain energy accumulated in the panel. Furthermore, overshoot occurring near the midchord can yield average temperatures and peak displacements exceeding those experienced by the panel subject to turbulent flow. Lastly, these results suggest that fully turbulent flow does not always conservatively predict the thermo-structural response of surface panels.},
doi = {10.2514/1.j054607},
journal = {AIAA Journal},
number = ,
volume = ,
place = {United States},
year = {Tue May 24 00:00:00 EDT 2016},
month = {Tue May 24 00:00:00 EDT 2016}
}
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Works referencing / citing this record:
Interplay of Surface Deformation and Shock-Induced Separation in Shock/Boundary-Layer Interactions
journal, December 2017
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