Author: William McKinley Davis
Publisher:
ISBN:
Category : Wind tunnels
Languages : en
Pages : 66
Book Description
Design Verification and Assembly of a Small, Demonstration Blowdown, Supersonic Wind Tunnel
Author: William McKinley Davis
Publisher:
ISBN:
Category : Wind tunnels
Languages : en
Pages : 66
Book Description
Publisher:
ISBN:
Category : Wind tunnels
Languages : en
Pages : 66
Book Description
The Design and Construction of a Small, Demonstration Blowdown, Supersonic Wind Tunnel
Author: F. Richard Folkerth
Publisher:
ISBN:
Category : Wind tunnels
Languages : en
Pages : 178
Book Description
Publisher:
ISBN:
Category : Wind tunnels
Languages : en
Pages : 178
Book Description
The design, construction, and calibration of a demonstration type supersonic wind tunnel
Author: James Carley Orr
Publisher:
ISBN:
Category : Wind tunnels
Languages : en
Pages : 230
Book Description
Publisher:
ISBN:
Category : Wind tunnels
Languages : en
Pages : 230
Book Description
The design and construction of a demonstration type supersonic wind tunnel
Author: Norman Sands
Publisher:
ISBN:
Category : Wind tunnels
Languages : en
Pages : 92
Book Description
Publisher:
ISBN:
Category : Wind tunnels
Languages : en
Pages : 92
Book Description
The Installation and Performance Evaluation of a Small Supersonic Wind Tunnel System
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
This report describes the procedure utilized in the assembly and evaluation of a small intermittent blowdown supersonic wind tunnel. The tunnel proper was fully constructed and nozzle blocks for attainment of a Mach number of 1.5 or 2.37 in the 0.5 by 1.718 in. test section were available. The basic schlieren system was purchased complete. An attempt was made to use or convert readily available materials for all components. It was expected that the results of this project would be of a permanent nature and would be utilized as a laboratory installation. The installation is suitable for the study of compressible fluid flow and the phenomenon of normal shocks but is not suitable for the study of the performance of shapes or models in the fluid flow. The tunnel installation operates satisfactorily with a maximum Mach number of 2.29 with approximately 0.28 lbm of air per second. Schlieren photographs of the flow field may be taken in either black and white or in color. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
This report describes the procedure utilized in the assembly and evaluation of a small intermittent blowdown supersonic wind tunnel. The tunnel proper was fully constructed and nozzle blocks for attainment of a Mach number of 1.5 or 2.37 in the 0.5 by 1.718 in. test section were available. The basic schlieren system was purchased complete. An attempt was made to use or convert readily available materials for all components. It was expected that the results of this project would be of a permanent nature and would be utilized as a laboratory installation. The installation is suitable for the study of compressible fluid flow and the phenomenon of normal shocks but is not suitable for the study of the performance of shapes or models in the fluid flow. The tunnel installation operates satisfactorily with a maximum Mach number of 2.29 with approximately 0.28 lbm of air per second. Schlieren photographs of the flow field may be taken in either black and white or in color. (Author).
The Installation and Performance Evaluation of a Small Supersonic Wind Tunnel System
Author: Charles O. Brown
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 96
Book Description
This report describes the procedure utilized in the assembly and evaluation of a small intermittent blowdown supersonic wind tunnel. The tunnel proper was fully constructed and nozzle blocks for attainment of a Mach number of 1.5 or 2.37 in the 0.5 by 1.718 in. test section were available. The basic schlieren system was purchased complete. An attempt was made to use or convert readily available materials for all components. It was expected that the results of this project would be of a permanent nature and would be utilized as a laboratory installation. The installation is suitable for the study of compressible fluid flow and the phenomenon of normal shocks but is not suitable for the study of the performance of shapes or models in the fluid flow. The tunnel installation operates satisfactorily with a maximum Mach number of 2.29 with approximately 0.28 lbm of air per second. Schlieren photographs of the flow field may be taken in either black and white or in color. (Author).
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 96
Book Description
This report describes the procedure utilized in the assembly and evaluation of a small intermittent blowdown supersonic wind tunnel. The tunnel proper was fully constructed and nozzle blocks for attainment of a Mach number of 1.5 or 2.37 in the 0.5 by 1.718 in. test section were available. The basic schlieren system was purchased complete. An attempt was made to use or convert readily available materials for all components. It was expected that the results of this project would be of a permanent nature and would be utilized as a laboratory installation. The installation is suitable for the study of compressible fluid flow and the phenomenon of normal shocks but is not suitable for the study of the performance of shapes or models in the fluid flow. The tunnel installation operates satisfactorily with a maximum Mach number of 2.29 with approximately 0.28 lbm of air per second. Schlieren photographs of the flow field may be taken in either black and white or in color. (Author).
Design Characteristics of a Blowdown Supersonic Wind Tunnel
Author: Juin Sheng Yu
Publisher:
ISBN:
Category :
Languages : en
Pages : 98
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 98
Book Description
The National union catalog, 1968-1972
Author:
Publisher:
ISBN:
Category : Union catalogs
Languages : en
Pages : 648
Book Description
Publisher:
ISBN:
Category : Union catalogs
Languages : en
Pages : 648
Book Description
Detailed Design of a Small Supersonic Wind Tunnel
Author: Thomas G. Piercy
Publisher:
ISBN:
Category :
Languages : en
Pages : 266
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 266
Book Description
The Design of a Small Supersonic Wind-tunnel
Author: Gary Arnold Flandro
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 80
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 80
Book Description