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E. Lara Lash
E. Lara Lash
University of Tennessee
Boundary layer
Mach number
Materials science
Mechanics
interaction studies
4
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2
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0
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Exploration of Upstream Influence and the Role of Shock Generator Geometry in Shock Wave/Transitional Boundary Layer Interactions at Mach 1.8 Edge Conditions
2020
E. Lara Lash
Mark Gragston
Zachary McDaniel
Phillip A. Kreth
John D. Schmisseur
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Preliminary Unsteady Characterization of Shock Wave/Boundary Layer Interactions on a 4% Scale SLS Model using uPSP and Shadowgraph
2020
E. Lara Lash
Nettie Roozeboom
Jennifer Baerny
Theodore J. Garbeff
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Withdrawal: Shockwave/Boundary-Layer Interaction Studies Performed in the NASA Langley 20-Inch Mach 6 Air Tunnel
2019
Brett F. Bathel
Stephen B. Jones
Neal Watkins
Scott A. Berry
Kyle Z. Goodman
William E. Lipford
Christopher S. Combs
John D. Schmisseur
Phillip A. Kreth
E. Lara Lash
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Withdrawal: Shockwave/Boundary-Layer Interaction Studies Performed in the NASA Langley 20-Inch Mach 6 Air Tunnel
2019
Brett F. Bathel
Stephen B. Jones
Neal Watkins
Scott A. Berry
Kyle Z. Goodman
William E. Lipford
Christopher S. Combs
John D. Schmisseur
Phillip A. Kreth
E. Lara Lash
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