2D analysis of tokamak divertor-plasma detachment-bifurcation with operational parameters and geometries by M. Zhao, F. Scotti, T.D. Rognlien, A.G. McLean, G. Burke, A. Holm

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PSEUDOSPECTRAL APPROXIMATION COMPARED WITH CONTROL VOLUME FORMULATION AND FINITE DIFFERENCES - SOME TEST CASES by ARTUR TYLISZCZAK, ANDRZEJ BOGUSŁAWSKI

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The modeling of two-dimensional vortex flows in a cylindrical channel using parallel calculations on a supercomputer by I. G. Lebo, I. V. Obruchev

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Visualization and Parameters Determination of Supersonic Flows in Convergent-Divergent Micro-Nozzles Using Schlieren Z-Type Technique and Fluid Mechanics by Reyna Judith Mendoza-Anchondo, Cornelio Alvarez-Herrera, José Guadalupe Murillo-Ramírez

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The impact of the Laval nozzle shape on thrust production, using the method of characteristics by Andrei - Ionut PARASCHIV

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Approximate Analytical Models of Shock-Wave Structure at Steady Mach Reflection by Mikhail V. Chernyshov, Karina E. Savelova, Anna S. Kapralova

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Effect of intermediate aerodisk mounted sharp tip spike on the drag reduction over a hemispherical body at Mach 2.0 by Tembhurnikar Payal V., Jadhav Akash T., Sahoo Devabrata

Subjects: “…supersonic flow…”
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Effect of size and location of an intermediate aerodisk mounted sharp tip spike on the drag reduction over a hemispherical body at mach 2.0 by Jadhav Akash T., Tembhurnikar Payal V., Bhosale Mrunal S., Nandy Jhumki, Sarwar Gulam M.D., Sahoo Devabrata

Subjects: “…supersonic flow…”
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NUMERICAL SIMULATION OF SHOCK WAVE PATTERNS IN SUPERSONIC DIVERGENT SYMMETRIC NOZZLES by KRYSTYNA NAMIEŚNIK, PIOTR DOERFFER

Subjects: “…supersonic flow…”
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Study of Transition to Turbulence in a Supersonic Boundary Layer Using DNS and Transition Prediction by Hiroshi MAEKAWA

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Effect of a Pylon Mounted Cavity-Based Flameholder on ‎the Combustor Flow Characteristics by S. Nayal, D. Sahoo

Subjects: “…supersonic flow; combustor performance; cavity flow; flameholder.…”
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Experimental Studies of Coaxial Jet Flows by Parviz BEHROUZI, James J. McGUIRK

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Numerical Simulation of Pressure Fluctuation near an Expansion Corner in a Supersonic Flow of M = 3.01 by Lei Zhang, Zi-Niu Wu

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Response of the Shock Wave/Boundary Layer Interaction to Disturbances Induced by the Plasma Discharge by Oleg Vishnyakov, Pavel Polivanov, Andrey Sidorenko

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Model for Wall Shear Stress from Obliquely Impinging Planar Underexpanded Jets by Patrick Fillingham, Arjun Viswanathan, Igor V. Novosselov

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Preliminary experiment of supersonic micro-channel gas flow visualization by using Interferometer by Yuya TAKAHASHI, Junnosuke OKAJIMA, Yuka IGA, Atsuki KOMIYA, Shigenao MARUYAMA

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Experimental study on the behavior of the two phase flow shock waves occurring in the ejector refrigeration cycle by Haruyuki NISHIJIMA, Kyohei TSUCHII, Masafumi NAKAGAWA

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Principles of Magnetohydrodynamical Control of Internal and External Supersonic Flows by Tatiana Lapushkina

Subjects: “…supersonic flow control…”
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Strategy to Apply DNS in a Supersonic Ejector by Karla Gonçalves Jacinto, Szabolcs Varga, Carlos Silva

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Usage of double injector for efficient mixing of the fuel behind the ramp injector at supersonic combustion chamber by Ihab Omar, Mohamed R. El-Sharkawy, Rifaqat Ali, Pradeep Kumar Singh, Husam Rajab, Mohsen Ahmed, Naim Ben Ali, Wajdi Rajhi, Lotfi Ben Said, S. Arman Abodollahi

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