Author: G. Fonda-Bonardi
Publisher:
ISBN:
Category :
Languages : en
Pages : 71
Book Description
An electrodeless plasma accelerator is described for use in simulating re-entry environments. Principles of its operation and a technical description of its several parts are given. Descriptions are given of the gas injector, pre-ionizer, magnetic structure, and cooling devices. Only enough of the theory of the accelerator operation necessary to a general understanding of the machine is included. (Author).
Development of an Alternating Current Plasma Accelerator for Application as an Ultra High Velocity Wind Tunnel
Author: G. Fonda-Bonardi
Publisher:
ISBN:
Category :
Languages : en
Pages : 71
Book Description
An electrodeless plasma accelerator is described for use in simulating re-entry environments. Principles of its operation and a technical description of its several parts are given. Descriptions are given of the gas injector, pre-ionizer, magnetic structure, and cooling devices. Only enough of the theory of the accelerator operation necessary to a general understanding of the machine is included. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 71
Book Description
An electrodeless plasma accelerator is described for use in simulating re-entry environments. Principles of its operation and a technical description of its several parts are given. Descriptions are given of the gas injector, pre-ionizer, magnetic structure, and cooling devices. Only enough of the theory of the accelerator operation necessary to a general understanding of the machine is included. (Author).
Development of Alternating Current Plasma Accelerator for Application as an Ultra-high-velocity Tunnel
Author: J. M. Rocard
Publisher:
ISBN:
Category : Plasma accelerators
Languages : en
Pages : 206
Book Description
The object of the research was to develop the technology required for the application of the continuous traveling wave concept to provide moving environment simulation of the conditions prevailing in the upper atmosphere between 300,000 and 400,000 feet altitude at velocities between 2,600 and 12,700 meters/sec. The efficient application of the travel concept to large wind tunnel facilites requires that polyphase tuned circuits be matched to appropriate power supplies and used to produce the traveling magnetic field. The design principles and prototype polyphase coil circuit and associated tuning circuitry are described in Section 3. The details of the prototype accelerator and associated power supplies are described in Section 4.
Publisher:
ISBN:
Category : Plasma accelerators
Languages : en
Pages : 206
Book Description
The object of the research was to develop the technology required for the application of the continuous traveling wave concept to provide moving environment simulation of the conditions prevailing in the upper atmosphere between 300,000 and 400,000 feet altitude at velocities between 2,600 and 12,700 meters/sec. The efficient application of the travel concept to large wind tunnel facilites requires that polyphase tuned circuits be matched to appropriate power supplies and used to produce the traveling magnetic field. The design principles and prototype polyphase coil circuit and associated tuning circuitry are described in Section 3. The details of the prototype accelerator and associated power supplies are described in Section 4.
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
Technical Abstract Bulletin
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 908
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 908
Book Description
U.S. Government Research Reports
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 2180
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 2180
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 584
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 584
Book Description
Proceedings
Author:
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 440
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 440
Book Description
Advanced Experimental Techniques for Study of Hypervelocity Flight
Author:
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 234
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 234
Book Description
ASD Technical Report
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 80
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 80
Book Description
New Research Frontiers in Physical Electronics
Author: University of Michigan. Department of Electrical Engineering
Publisher:
ISBN:
Category : Electrical engineering
Languages : en
Pages : 340
Book Description
Publisher:
ISBN:
Category : Electrical engineering
Languages : en
Pages : 340
Book Description