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

Joseph S. Jewell

U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433

*Research Aerospace Engineer (NRC Research Associate), AFRL/RQHF; . Senior Member AIAA.

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Nicholaus J. Parziale

Stevens Institute of Technology, Hoboken, New Jersey 07030

†Assistant Professor, Mechanical Engineering, Castle Point on Hudson. Member AIAA.

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Ivett A. Leyva

U.S. Air Force Office of Scientific Research, Arlington Air Force Base, Virginia 22203

‡Program Officer, AFOSR/RTE. Associate Fellow AIAA.

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and

Joseph E. Shepherd

California Institute of Technology, Pasadena, California 91125

§Professor, Graduate Aeronautical Laboratories, 1200 E. California Blvd., MC 105-50. Senior Member AIAA.

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Published Online:16 Sep 2016https://doi.org/10.2514/1.J054897

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Volume 55, Number 1January 2017

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Acknowledgments

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 CO2/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.

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Received17 November 2015
Accepted4 July 2016
Published online16 September 2016

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

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