Author: Gloyd A. Simmons
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Electron Attachment in Seeded Air for Hypervelocity MHD Accelerator Propulsion Wind Tunnel Applications
34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 636
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 636
Book Description
30th Plasmadynamics and Lasers Conference
Author:
Publisher:
ISBN:
Category : Lasers
Languages : en
Pages : 470
Book Description
Publisher:
ISBN:
Category : Lasers
Languages : en
Pages : 470
Book Description
International Aerospace Abstracts
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1032
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1032
Book Description
Development of a Continuous Flow Electromagnetic Alternating Current Traveling Wave Accelerator for High-density, Hypervelocity Wind Tunnel Applications
Author: John A. Thornton
Publisher:
ISBN:
Category : Electric waves
Languages : en
Pages : 136
Book Description
Publisher:
ISBN:
Category : Electric waves
Languages : en
Pages : 136
Book Description
29th Plasmadynamics and Lasers Conference
Author:
Publisher:
ISBN:
Category : Lasers
Languages : en
Pages : 434
Book Description
Publisher:
ISBN:
Category : Lasers
Languages : en
Pages : 434
Book Description
A Feasibility Study and Experimental Evaluation on MHD Acceleration for Application to Advanced Propulsion and Hypervelocity Ground Testing
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 34
Book Description
This report results from a contract tasking Russian Academy of Sciences as follows: The contractor will conduct initial feasibility and analysis studies on the application of MHD accelerator for propulsion and flow acceleration. The overall objective of the proposed project is to perform preliminary testing in order to evaluate an experimental MHD accelerator laboratory that can be used in the future for both experimentation into MHD propulsion and as a hypervelocity wind tunnel for experiments into hypersonic flow and flight control system within the confines of the proposed program, the contractor seeks to: a) analyze and report on the potential capability of MHO acceleration assisted advanced propulsion and to provide quasi-steady state hypervelocity ground tests; 2) evaluate an existing experimental MHD accelerator laboratory for experimental testing and 3) develop an experimental plan for conduct of an open demonstration experiment.
Publisher:
ISBN:
Category :
Languages : en
Pages : 34
Book Description
This report results from a contract tasking Russian Academy of Sciences as follows: The contractor will conduct initial feasibility and analysis studies on the application of MHD accelerator for propulsion and flow acceleration. The overall objective of the proposed project is to perform preliminary testing in order to evaluate an experimental MHD accelerator laboratory that can be used in the future for both experimentation into MHD propulsion and as a hypervelocity wind tunnel for experiments into hypersonic flow and flight control system within the confines of the proposed program, the contractor seeks to: a) analyze and report on the potential capability of MHO acceleration assisted advanced propulsion and to provide quasi-steady state hypervelocity ground tests; 2) evaluate an existing experimental MHD accelerator laboratory for experimental testing and 3) develop an experimental plan for conduct of an open demonstration experiment.
Magnetohydrodynamics Accelerator Research Into Advanced Hypersonics (MARIAH)
Author:
Publisher:
ISBN:
Category : Gas dynamics
Languages : en
Pages : 444
Book Description
Publisher:
ISBN:
Category : Gas dynamics
Languages : en
Pages : 444
Book Description
Magnetohydrodynamics Accelerator Research Into Advanced Hypersonics (MARIAH)
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 658
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 658
Book Description
Mhd Generator and Accelerator Experiments in Seeded and Unseeded Air Flows
Author: Clarence J. Harris
Publisher:
ISBN:
Category :
Languages : en
Pages : 31
Book Description
Two types of MHD experiments were conducted using air flows produced by hypersonic shock tunnels. One experimental program was designed to evaluate the feasibility of using the Lorenz forces developed in an MHD generator for the attitude control of a hypervelocity vehicle. During this study the electrical conductivity of the seeded shock layer flow about a blunt model located in the shock tunnel test section was investigated along with the effect of pre-heating the generator electrodes. In the second experimental program, a Faraday accelerator is being studied to determine its ability to add kinetic energy to a high density, unseeded air flow in a high enthalpy shock tunnel. Measurements were made of the gross electrical conductivity of the flow, with and without an applied magnetic field. The meaning of the electrical conductivity measurements for each of these experiments is discussed.
Publisher:
ISBN:
Category :
Languages : en
Pages : 31
Book Description
Two types of MHD experiments were conducted using air flows produced by hypersonic shock tunnels. One experimental program was designed to evaluate the feasibility of using the Lorenz forces developed in an MHD generator for the attitude control of a hypervelocity vehicle. During this study the electrical conductivity of the seeded shock layer flow about a blunt model located in the shock tunnel test section was investigated along with the effect of pre-heating the generator electrodes. In the second experimental program, a Faraday accelerator is being studied to determine its ability to add kinetic energy to a high density, unseeded air flow in a high enthalpy shock tunnel. Measurements were made of the gross electrical conductivity of the flow, with and without an applied magnetic field. The meaning of the electrical conductivity measurements for each of these experiments is discussed.