Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 60
Book Description
Normal Injection of Helium from Swept Struts Into Ducted Supersonic Flow
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 60
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 60
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 970
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 : 970
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.
Study of Injection of Helium Into Supersonic Air Flow Using Rayleigh Scattering
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
Book Description
Experimental Investigation of Helium Injection at a Low Downstream Angle Into Supersonic Flow
Author: Richard Bruce Mays
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 384
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 384
Book Description
Study of injection of helium into supersonic air flow using Rayleigh scattering
Author: Richard G. Seasholtz
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 12
Book Description
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 12
Book Description
Aeronautical Engineering
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 640
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 : 640
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)
Government Reports Annual Index
Author:
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 882
Book Description
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 882
Book Description
Government Reports Index
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1014
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1014
Book Description
A Study of Secondary Injection of Gases Into a Supersonic Flow
Author: R. Rosen
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 82
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 82
Book Description
An Analytical and Experimental Investigation of the Annular Injection of Helium Into a Supersonic Air Core
Author: Clarence Albert Kemper
Publisher:
ISBN:
Category :
Languages : en
Pages : 208
Book Description
When a lightweight gas is injected into the boundary layer of a high-speed air flow, the adiabatic wall temperature is reduced by means of a change in properties of the gas in the region where viscous dissipation occurs. The paper summarizes some of the results of a controlled experiment in which helium was injected through an annular slot and along the impermeable surface of a 1.46 inch diameter tube in which a supersonic air stream was flowing at a Mach number of about 4.8. A discussion of some of the analytical results which were obtained is also given. The experimental portion of the investigation included the development of miniaturized boundary layer instrumentation capable of measuring velocity, temperature, and concentration profiles of the flow.
Publisher:
ISBN:
Category :
Languages : en
Pages : 208
Book Description
When a lightweight gas is injected into the boundary layer of a high-speed air flow, the adiabatic wall temperature is reduced by means of a change in properties of the gas in the region where viscous dissipation occurs. The paper summarizes some of the results of a controlled experiment in which helium was injected through an annular slot and along the impermeable surface of a 1.46 inch diameter tube in which a supersonic air stream was flowing at a Mach number of about 4.8. A discussion of some of the analytical results which were obtained is also given. The experimental portion of the investigation included the development of miniaturized boundary layer instrumentation capable of measuring velocity, temperature, and concentration profiles of the flow.