Publications

PhD Thesis


Shock-Induced Separation of Transitional Hypersonic Boundary Layers. Imperial College London. 2015.

https://spiral.imperial.ac.uk:8443/handle/10044/1/24803

Side Projects and Fun Stuff


Joe Linger, Leon Vanstone and Ravi Lumba (2016). Developing a Mass Standard for Planetary Landings

https://www.dropbox.com/s/xa9hamsyupff7mr/Joe%20Lingren%20-%20Lingren_Joe_PAPERv3.docx?dl=0

 

 

 

Journal Articles


Estruch-Samper, Vanstone, Hillier & Ganapathisubramani (2014). Micro vortex generator control of axisymmetric high-speed laminar boundary layer separation. Shock Waves J.

http://link.springer.com/article/10.1007/s00193-014-0514-7

 

Estruch-Samper, L. Vanstone, R. Hillier, B. Ganapathisubramani (2015). Toluene-based planar laser-induced fluorescence imaging of temperature in hypersonic flows. Experiments in Fluids.

http://link.springer.com/article/10.1007%2Fs00348-015-1987-6

 

 

Conference Proceedings


Estruch-Samper, D., Vanstone, L., Ganapathisubramani, B., & Hillier, R. (2012). Axisymmetric flare-induced separation of high-speed transitional boundary layers. AIAA.

http://arc.aiaa.org/doi/abs/10.2514/6.2012-67

 

Vanstone, L., Estruch-Samper, D., Ganapathisubramani, B., & Hillier, R. (2013). Shock Induced Boundary Layer Separation of Transitional Hypersonic Boundary Layers. AIAA.

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2736

 

Vanstone, L., Saleem, M., Seckin, S., Clemens, N. (2015). Experimental Investigation of Unsteadiness of Swept-Ramp Shock/Boundary Layer Interactions at Mach 2. AIAA.

http://arc.aiaa.org/doi/abs/10.2514/6.2015-2932

 

Hillier, R., Estruch-Samper, D., Murray, N., Vanstone, L. & Williams, S. (2015). Gun Tunnel Studies of Shock-Wave/Boundary-Layer Interactions: Laminar, Transitional and Turbulent. John Stollery Invited Lecture. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference (Hypersonics 2015).

http://arc.aiaa.org/doi/abs/10.2514/6.2015-3512

 

Vanstone, L., Saleem, M., Seckin, S., Clemens, N. Due 2016. High-Speed Imaging of Swept-Ramp Shock/Boundary Layer Interactions at Mach 2. AIAA SciTech 2016