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An analytical and experimental study of a hybrid rocket motor

Type: Journal Paper

Author : H. Rezaei; M. R. Soltani

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Performance study of an inlet in supersonic flow

Type: Journal Paper

Author : M. R. Soltani; M. Farahani

Year: 2012

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Experimental Investigation of Effects of Mach Number on the Flow Instability in a Supersonic Inlet

Type: Journal Paper

Author : M.R. Soltani; M. Farahani

Year: 2012

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Effect of amplitude and mean angle-of-attack on the boundary layer of an oscillating aerofoil

Type: Journal Paper

Author : M. R. Soltani; A. Bakhshalipour

Year: 2008

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Effect of amplitude and mean angle-of-attack on the boundary layer of an oscillating aerofoil

Type: Journal Paper

Author : M. R. Soltani; A. Bakhshalipour

Year: 2008

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Experimental study of the boundary layer over an airfoil in plunging motion

Type: Journal Paper

Author : F. Rasi Marzabadi, M. R. Soltani

Year: 2012

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Numerical Simulation of Mixed Compression Intake Buzz

Type: Journal Paper

Author : M. R. Soltani; M. Abedi; R. Askari

Year: 2017

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Entanglement in a two-spin system with long-range interactions

Type: Journal Paper

Author : M R Soltani; S Mahdavifar; M Mahmoudi

Year: 2016

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Investigation of the pressure distribution and transition point over a swept wing

Type: Journal Paper

Author : M.R. Soltani; K. Ghorbanian; M. Masdari

Year: 2011

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Early vortex burst on a delta wing in pitch

Type: Journal Paper

Author : M. R. Soltani; M. B. Bragg

Year: 1993

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An analytical and experimental study of a hybrid rocket motor

Performance study of an inlet in supersonic flow

Experimental Investigation of Effects of Mach Number on the Flow Instability in a Supersonic Inlet

Effect of amplitude and mean angle-of-attack on the boundary layer of an oscillating aerofoil

Effect of amplitude and mean angle-of-attack on the boundary layer of an oscillating aerofoil

Experimental study of the boundary layer over an airfoil in plunging motion

Numerical Simulation of Mixed Compression Intake Buzz

Entanglement in a two-spin system with long-range interactions

Investigation of the pressure distribution and transition point over a swept wing

Early vortex burst on a delta wing in pitch

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An analytical and experimental study of a hybrid rocket motor

Performance study of an inlet in supersonic flow

Experimental Investigation of Effects of Mach Number on the Flow Instability in a Supersonic Inlet

Effect of amplitude and mean angle-of-attack on the boundary layer of an oscillating aerofoil

Effect of amplitude and mean angle-of-attack on the boundary layer of an oscillating aerofoil

Experimental study of the boundary layer over an airfoil in plunging motion

Numerical Simulation of Mixed Compression Intake Buzz

Entanglement in a two-spin system with long-range interactions

Investigation of the pressure distribution and transition point over a swept wing

Early vortex burst on a delta wing in pitch