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Julio Srulijes

Observed names: J Srulijes, J. SRULIJES, J. Srulijes, Srulijes, J., Srulijes, Julio
OpenAlex ID: A5069320461
Flowfield Around Spike-Tipped Bodies for High Attack Angles at Mach 4.5
2003 · P. Gnemmi, J. Srulijes, et al. · Journal of Spacecraft and Rockets · 75
Novel Sensor for Fast Heat Flux Measurements
2009 · Helmut Knauss, Tim Roediger, et al. · Journal of Spacecraft and Rockets · 67
A Novel Sensor for Fast Heat Flux Measurements
2006 · Helmut Knauss, Tim Roediger, et al. · AIAA Aerodynamic Measurement Technology and Ground Testing Conference · 24
High-Pressure Shock Tunnel Experiments and CFD Calculations on Spike-Tipped Blunt Bodies
2002 · Julio Srulijes, Patrick Gnemmi, et al. · AIAA Aerodynamic Measurement Technology and Ground Testing Conference · 21
Expansion tube experiments for the investigation of ram-accelerator-related combustion and gasdynamic problems
1992 · J. SRULIJES, G. SMEETS, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 19
Mach waves produced in the supersonic jet mixing layer by shock/vortex interaction
2016 · H. Oertel Sen, F. Seiler, et al. · Shock Waves · 16
Presentation of the rail tube version II of ISL’s RAMAC 30
1998 · F. Seiler, G. Patz, et al. · Springer eBooks · 16
Heat Fluxes Inside a Cavity Placed at the Nose of a Projectile Measured in a Shock Tunnel at Mach 4.5
2007 · F. Seiler, J. Srulijes, et al. · Springer eBooks · 14
Determination of Aerodynamic Coefficients from Shock Tunnel Free Flight Trajectories
2012 · Pierre Wey, Friedrich Seiler, et al. · AIAA Aerodynamic Measurement Technology and Ground Testing Conference · 13
Visualization of Mach waves produced by a supersonic jet and theoretical explanations
2013 · H. Oertel Sen, F. Seiler, et al. · Journal of Visualization · 12
Shock tunnel high-speed photography and CFD calculations on spike-tipped bodies
2003 · Julio Srulijes, Patrick Gnemmi, et al. · Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE · 10
Flow field around spike-tipped bodies
2001 · P. Gnemmi, J. Srulijes, et al. · AIAA Applied Aerodynamics Conference · 9
New Explanation of Noise Production by Supersonic Jets with Gas Dredging
2010 · H. Oertel Sen, F. Seiler, et al. · Notes on numerical fluid mechanics and multidisciplinary design · 8
Progress of ram acceleration with ISL's RAMAC 30
2000 · F. Seiler, G. Patz, et al. · Journal de Physique IV (Proceedings) · 8
Progress in Doppler picture velocimetry (DPV)
2008 · F. Seiler, A. George, et al. · Experiments in Fluids · 7
Planar velocity visualization in high-speed wedge flow using Doppler Picture Velocimetry (DPV) compared with Particle Image Velocimetry (PIV)
2003 · F. Seiler, M. Havermann, et al. · Journal of Visualization · 7
Flow velocities visualization using Doppler picture interference velocimetry
2003 · F. Seiler, A. George, et al. · International Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF) · 7
Doppler-pictures of velocity fields - An application to fluid mechanics
1986 · F. Seiler, J. Srulijes · 7
The behaviour of fin-guided projectiles superdetonative accelerated in ISL’s RAMAC 30
1998 · G. Patz, F. Seiler, et al. · Springer eBooks · 6
A Doppler-picture camera for velocity field visualization
1987 · F. Seiler, J. Srulijes, et al. · 6
Vortices And Pressure Waves At Trailing Edges
1985 · F. Seiler, J. Srulijes · Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE · 6
Vortex Induced Mach Waves in Supersonic Jets
2012 · H. Oertel Sen, F. Seiler, et al. · Springer eBooks · 5
Experimental simulation of airbag deployment for pipeline closing
2005 · F. Seiler, H. Ende, et al. · Journal of Loss Prevention in the Process Industries · 5
Separation of fluid phases and bubble dynamics in a temperature gradient - A spacelab D 1 experiment
1987 · R. Naehle, David Neuhaus, et al. · Zeitschrift für Flugwissenschaften und Weltraumforschung · 5
Shock Tunnels at ISL
2015 · Patrick Gnemmi, Julio Srulijes, et al. · Springer eBooks · 4
Works count: 76
Citation count: 428
H-index: 10
I10-index: 11
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