Performance Theory of Diagonal Conducting Wall  Magnetohydrodynamic Accelerators

Litchford, Ron J.

doi:10.2514/1.3698

Cited by 3 publications

References 15 publications

(14 reference statements)

Supporting

Mentioning

Contrasting

Order By: Relevance

Status of Magnetohydrodynamic Augmented Propulsion Experiment

Litchford

Lineberry

2007

38th Plasmadynamics and Lasers Conference

View full text Add to dashboard Cite

Over the past several years, efforts have been under way to design and develop an operationaUy flexible research facility for investigating the use of cross-field MHO accelerators as a potential thrust augmentation device for tbermal propulsion systems, The baseline configuration for this high-power experimental facility utilizes a 1,5-MW, multi-gas arc-heater as a thermal driver for a 2-MW, MHO accelerator, which resides in a large-bore 2-tesla electromagnet. A preliminary design study using NaK seeded nitrogen as tbe working fluid Jed to an eIternaUy dlagonalized segmented MHI> cbannel configuration based on an expendable beat-sink desigu concept. Tbe current status report includes a review of engineering/design work and performance optimization analyses and summarizes component bardware fabrication and development efforts, preliminary testing results, and recent progress toward full-up assembly and testing

show abstract

Status of Magnetohydrodynamic Augmented Propulsion Experiment

Litchford

Lineberry

2007

38th Plasmadynamics and Lasers Conference

View full text Add to dashboard Cite

show abstract

Three-Dimensional Numerical Modeling of the Magnetohydrodynamic Augmented Propulsion Experiment

Turner

Hawk

Litchford

2008

46th AIAA Aerospace Sciences Meeting and Exhibit

View full text Add to dashboard Cite

Progress in Hypersonic Inlet Flow Controls by Magnetohydrodynamic

Zhang

Hong

Zhang

et al. 2015

AMM

View full text Add to dashboard Cite

The magnetohydrodynamic (MHD) flow control techniques for inlet based on “AJAX” vehicle concept have attracted many researchers’ attention for its potential wide applications in the supersonic flights or the hypersonic ones. In this paper, a preliminary discussion for basic problems that are ionization and magnetic field in the MHD applications is presented. And three major MHD techniques for enhancing inlet aerodynamic performance and operability, which are large scale flow control for enlarging flight scope in Mach/angle-of-attack, near surface flow control for shock wave/boundary layer interaction and leading edge heating-transfer control for enormous thermal load on leading edge of the compression ramp, are briefly explained and reviewed.

show abstract

Performance Theory of Diagonal Conducting Wall Magnetohydrodynamic Accelerators

Cited by 3 publications

References 15 publications

Status of Magnetohydrodynamic Augmented Propulsion Experiment

Status of Magnetohydrodynamic Augmented Propulsion Experiment

Three-Dimensional Numerical Modeling of the Magnetohydrodynamic Augmented Propulsion Experiment

Progress in Hypersonic Inlet Flow Controls by Magnetohydrodynamic

Contact Info

Product

Resources

About