Author: Joel Moshe Avidor Oberndorfer
Publisher:
ISBN:
Category : Aerodynamcis, Hypersonic
Languages : en
Pages : 220
Book Description
Flow Field Diagnostics in Rarefied Slightly Ionized Hypersonic Flow
Author: Joel Moshe Avidor Oberndorfer
Publisher:
ISBN:
Category : Aerodynamcis, Hypersonic
Languages : en
Pages : 220
Book Description
Publisher:
ISBN:
Category : Aerodynamcis, Hypersonic
Languages : en
Pages : 220
Book Description
Flow Field Diagnostics in Rarefied Slightly Ionized Hypersonic Flow
Author: Joel M. Avidor
Publisher:
ISBN:
Category :
Languages : en
Pages : 125
Book Description
An experimental investigation was carried out in the hypersonic shock tunnel in which two diagnostic techniques, the cylindrical electrostatic probe and the electron beam density probe, were applied to flow field surveys in rarefied slightly ionized hypersonic flow. Their relative merits have been evaluated. It was found that both can be applied for flow field investigations and particularly, density tracing and mapping, provided that diffusion effects are nonexistent or negligible. In the course of this work, ion and neutral density profiles normal to a sharp flat plate and in the near wake of a 10 deg half angle cone were obtained. Also using flush electrostatic probes, the ambipolar diffusion flux of the ionized particles to the plate was measured. A comparison with theoretical results obtained using the Rudman-Rubin formulation for the hypersonic flow about a sharp flat plate modified for slightly ionized flow was carried out. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 125
Book Description
An experimental investigation was carried out in the hypersonic shock tunnel in which two diagnostic techniques, the cylindrical electrostatic probe and the electron beam density probe, were applied to flow field surveys in rarefied slightly ionized hypersonic flow. Their relative merits have been evaluated. It was found that both can be applied for flow field investigations and particularly, density tracing and mapping, provided that diffusion effects are nonexistent or negligible. In the course of this work, ion and neutral density profiles normal to a sharp flat plate and in the near wake of a 10 deg half angle cone were obtained. Also using flush electrostatic probes, the ambipolar diffusion flux of the ionized particles to the plate was measured. A comparison with theoretical results obtained using the Rudman-Rubin formulation for the hypersonic flow about a sharp flat plate modified for slightly ionized flow was carried out. (Author).
Slightly Ionized Low Density Hypersonic Flow about a Sharp Plate and Its Diagnostics
Author: Joel M. Avidor
Publisher:
ISBN:
Category :
Languages : en
Pages : 13
Book Description
An experimental investigation is reported in a hypersonic shock tunnel in which two diagnostic techniques, the cylindrical electrostatic probe and the electron beam density probe, were applied to flow field surveys in rarefied slightly ionized hypersonic flow. Ion and neutral density profiles normal to a sharp flat plate at M =18 were obtained. Also, using flush electrostatic probes, the ambipolar diffusion flux of the ionized particles to the plate was measured. A comparison with numerical results was obtained. In the viscous layer; large deviations were observed between the measured and calculated maximum density. No agreement was found to exist between ion and neutral density profiles normal to the plate. (Modified author abstract).
Publisher:
ISBN:
Category :
Languages : en
Pages : 13
Book Description
An experimental investigation is reported in a hypersonic shock tunnel in which two diagnostic techniques, the cylindrical electrostatic probe and the electron beam density probe, were applied to flow field surveys in rarefied slightly ionized hypersonic flow. Ion and neutral density profiles normal to a sharp flat plate at M =18 were obtained. Also, using flush electrostatic probes, the ambipolar diffusion flux of the ionized particles to the plate was measured. A comparison with numerical results was obtained. In the viscous layer; large deviations were observed between the measured and calculated maximum density. No agreement was found to exist between ion and neutral density profiles normal to the plate. (Modified author abstract).
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1460
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1460
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Nuclear Science Abstracts
Research in Progress
Applied Mechanics Reviews
Government Reports Index
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1120
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1120
Book Description
Aeronautical Engineering
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 932
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 932
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).