AbstractThis paper presents a preliminary experimental investigation on magnetohydrodynamic (MHD) power generation using seeded supersonic argon flow as working fluid. Helium and argon are used as driver and driven gas respectively in a shock tunnel. Equilibrium contact surface operating mode is used to obtain high temperature gas, and the conductivity is obtained by adding seed K2CO3 powder into the driven section. Under the conditions of nozzle inlet total pressure being 0.32 MPa, total temperature 6 504 K, magnetic field density about 0.5 T and nozzle outlet velocity 1 959 m/s, induction voltage and short-circuit current of the segmentation MHD power generation channel are measured, and the experimental results agree with theoretical cal...
The prospects for realizing a magnetohydrodynamic (MHD) bypass hypersonic airbreathing engine are ex...
The interaction between high-enthalpy partially ionized gas flows and magnetic fields, mostly called...
Calculations of preionized plasma flow with finite recombination rate - magnetohydrodynamic power ge...
AbstractThis paper presents a preliminary experimental investigation on magnetohydrodynamic (MHD) po...
Historically, the National Aeronautics and Space Administration (NASA) has used rocket-powered vehic...
AbstractMagnetohydrodynamic (MHD) power generation with supersonic non-equilibrium plasma is demonst...
Over the past several years, efforts have been under way to design and develop an operationally flex...
A novel concept of hypersonic cold-air MHD power generators is discussed. Ionization of the cold air...
At the beginning of the seventies, experimental research using short duration supersonic shock drive...
An experimental MHD generator facility is described, in which cesium-seeded argon is used as a worki...
Magnetohydrodynamic (MHD) power generation with supersonic non-equilibrium plasma is demonstrated. C...
Hypersonic flight using scramjet propulsion bridges the gap between turbojets and rockets. Recent ef...
The present program was conducted by the University of Tennessee Space Institute (UTSI). It was by i...
The research project studied the benefits of Magnetogasdynamic (MGD) acceleration on a scramjet nozz...
A detailed computational analysis of the flow in, and power extraction from, a combustion-driven, MH...
The prospects for realizing a magnetohydrodynamic (MHD) bypass hypersonic airbreathing engine are ex...
The interaction between high-enthalpy partially ionized gas flows and magnetic fields, mostly called...
Calculations of preionized plasma flow with finite recombination rate - magnetohydrodynamic power ge...
AbstractThis paper presents a preliminary experimental investigation on magnetohydrodynamic (MHD) po...
Historically, the National Aeronautics and Space Administration (NASA) has used rocket-powered vehic...
AbstractMagnetohydrodynamic (MHD) power generation with supersonic non-equilibrium plasma is demonst...
Over the past several years, efforts have been under way to design and develop an operationally flex...
A novel concept of hypersonic cold-air MHD power generators is discussed. Ionization of the cold air...
At the beginning of the seventies, experimental research using short duration supersonic shock drive...
An experimental MHD generator facility is described, in which cesium-seeded argon is used as a worki...
Magnetohydrodynamic (MHD) power generation with supersonic non-equilibrium plasma is demonstrated. C...
Hypersonic flight using scramjet propulsion bridges the gap between turbojets and rockets. Recent ef...
The present program was conducted by the University of Tennessee Space Institute (UTSI). It was by i...
The research project studied the benefits of Magnetogasdynamic (MGD) acceleration on a scramjet nozz...
A detailed computational analysis of the flow in, and power extraction from, a combustion-driven, MH...
The prospects for realizing a magnetohydrodynamic (MHD) bypass hypersonic airbreathing engine are ex...
The interaction between high-enthalpy partially ionized gas flows and magnetic fields, mostly called...
Calculations of preionized plasma flow with finite recombination rate - magnetohydrodynamic power ge...