AIAA-2019-2904: Shockwave/Boundary-Layer Interaction Studies Performed in the NASA Langley 20-Inch Mach 6 Air Tunnel
Ground testing (Conference)

Authors: Bathel, Brett F., Jones, Stephen B., Watkins, Anthony N., Berry, Scott, Goodman, Kyle, Combs, Christopher S., Schmisseur, John D., Kreth, Phillip A., Lash, E. Lara

Source: Papers American Institute of Aeronautics and Astronautics. 2806-3725:138-152

Availability: http://explore.bl.uk/primo_library/libweb/action/display.do?tabs=detailsTab&gathStatTab=true&ct=display&fn=search&doc=ETOCCN605587444&indx=1&recIds=ETOCCN605587444

Study of the Dynamics of Transitional Shock Wave-Boundary Layer Interactions using Optical Diagnostics (AIAA 2017-3123)
Fluid dynamics (Conference)

Authors: Lash, E. Lara, Combs, Christopher S., Kreth, Phillip A., Schmisseur, John D.

Source: Papers American Institute of Aeronautics and Astronautics. 3114-3463:150-171

Availability: http://explore.bl.uk/primo_library/libweb/action/display.do?tabs=detailsTab&gathStatTab=true&ct=display&fn=search&doc=ETOCCN602679237&indx=1&recIds=ETOCCN602679237

Experimental Investigation of a Cylinder-Induced Transitional Shock Wave-Boundary Layer Interaction (AIAA 2017-0760)
55th AIAA Aerospace Sciences Meeting 2017

Authors: Lash, E. Lara, Combs, Christopher S., Kreth, Phillip A., Schmisseur, John D.

Source: Papers American Institute of Aeronautics and Astronautics. 0543-0986:8191-8214

Availability: http://explore.bl.uk/primo_library/libweb/action/display.do?tabs=detailsTab&gathStatTab=true&ct=display&fn=search&doc=ETOCCN602580633&indx=1&recIds=ETOCCN602580633

Developing an Image-Based Analysis of the Dynamics of Transitional Shock Wave-Boundary Layer Interactions (AIAA 2016-4320)
32nd AIAA aerodynamic measurement technology and ground testing conference 2016

Authors: Lash, E. Lara, Combs, Christopher S., Kreth, Phillip A., Beckman, Emily A., Schmisseur, John D.

Source: Papers American Institute of Aeronautics and Astronautics. 3109-4112:478-492

Availability: http://explore.bl.uk/primo_library/libweb/action/display.do?tabs=detailsTab&gathStatTab=true&ct=display&fn=search&doc=ETOCCN601838460&indx=1&recIds=ETOCCN601838460

Investigation of a Cylinder-Induced Transitional Shock Wave-Boundary Layer Interaction using Laser Diagnostics (AIAA 2016-4321)
32nd AIAA aerodynamic measurement technology and ground testing conference 2016

Authors: Combs, Christopher S., Lash, E. Lara, Schmisseur, John D.

Source: Papers American Institute of Aeronautics and Astronautics. 3109-4112:493-513

Availability: http://explore.bl.uk/primo_library/libweb/action/display.do?tabs=detailsTab&gathStatTab=true&ct=display&fn=search&doc=ETOCCN601838471&indx=1&recIds=ETOCCN601838471

Upstream Influence in Shock Wave/Transitional Boundary Layer Interactions at Mach 1.8.

Authors: Lash, E. Lara¹, Gragston, Mark², Kreth, Phillip A.³, McDaniel, Zachary⁴, Coder, James G.⁵, Schmisseur, John D.⁶

Source: AIAA Journal. Dec2021, Vol. 59 Issue 12, p4842-4857. 16p.

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