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Effects of Shock-Tube Cleanliness on Hypersonic Boundary Layer Transition at High Enthalpy

Jewell, Joseph S. and Parziale, Nicholaus J. and Leyva, Ivett A. and Shepherd, Joseph E. (2017) Effects of Shock-Tube Cleanliness on Hypersonic Boundary Layer Transition at High Enthalpy. AIAA Journal, 55 (1). pp. 332-338. ISSN 0001-1452. https://resolver.caltech.edu/CaltechAUTHORS:20170216-123740900

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Abstract

The prediction of a high-speed boundary-layer transition (BLT) location is critical to hypersonic vehicle design; this is because the increased skin friction and surface heating rate after transition result in increased weight of the thermal protection system. Experimental studies using hypervelocity wind tunnels are one component of BLT research.


Item Type:Article
Related URLs:
URLURL TypeDescription
http://dx.doi.org/10.2514/1.J054897DOIArticle
http://arc.aiaa.org/doi/10.2514/1.J054897PublisherArticle
ORCID:
AuthorORCID
Jewell, Joseph S.0000-0002-4047-9998
Parziale, Nicholaus J.0000-0001-9880-1727
Shepherd, Joseph E.0000-0003-3181-9310
Additional Information:This material is declared a work of the U.S. Government and is not subject to copyright protection in the United States. Presented as Paper 2015-1786 at the 53rd AIAA Aerospace Sciences Meeting, Kissimmee, FL, 5–9 January 2015; received 17 November 2015; revision received 30 June 2016; accepted for publication 4 July 2016; published online 14 September 2016. This work was an activity that was part of the National Center for Hypersonic Laminar-Turbulent Research, sponsored by the “Integrated Theoretical, Computational, and Experimental Studies for Transition Estimation and Control” project, supported by the U.S. Air Force Office of Scientific Research and NASA (FA9552-09-1-0341). Additionally, this work was part of the “Transition Delay in Hypervelocity Boundary Layers by Means of CO2CO2/Acoustic Interactions” project, sponsored by the U.S. Air Force Office of Scientific Research (FA9550-10-1-0491). J. S. Jewell received additional support from the National Defense Science and Engineering Graduate Fellowship, the Jack Kent Cooke Foundation, and the National Research Council Research Associateship. The authors would like to thank Bahram Valiferdowsi (California Institute of Technology) for help running T5, Ross Wagnild (Sandia National Laboratories) for help with the program to compute the run conditions, and Elizabeth Jewell (University of Michigan) for statistical advice.
Group:GALCIT
Funders:
Funding AgencyGrant Number
Air Force Office of Scientific Research (AFOSR)FA9552-09-1-0341
NASAUNSPECIFIED
Air Force Office of Scientific Research (AFOSR)FA9550-10-1-0491
National Defense Science and Engineering Graduate (NDSEG) FellowshipUNSPECIFIED
Jack Kent Cooke FoundationUNSPECIFIED
National Research CouncilUNSPECIFIED
Other Numbering System:
Other Numbering System NameOther Numbering System ID
AIAA Paper2015-1786
Issue or Number:1
Record Number:CaltechAUTHORS:20170216-123740900
Persistent URL:https://resolver.caltech.edu/CaltechAUTHORS:20170216-123740900
Official Citation:Joseph S. Jewell, Nicholaus J. Parziale, Ivett A. Leyva, Joseph E. Shepherd. "Effects of Shock-Tube Cleanliness on Hypersonic Boundary Layer Transition at High Enthalpy", AIAA Journal, Vol. 55, No. 1 (2017), pp. 332-338. http://dx.doi.org/10.2514/1.J054897
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:74379
Collection:CaltechAUTHORS
Deposited By: George Porter
Deposited On:16 Feb 2017 21:36
Last Modified:03 Oct 2019 16:38

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