Author: William W. Willmarth
Publisher:
ISBN:
Category :
Languages : en
Pages : 23
Book Description
The structure of the fluctuating flow field in a turbulent boundary layer has been investigated with the aid of extremely small hot wire probes. Two investigations were conducted. In one investigations of a small X array hot-wire probe, with dimensions (length and spacing) of the order of 2.5 viscous lengths (100 Microns) was constructed and used to measure the small scale structure of the velocity fluctuations and the Reynolds stress near the wall. It was found that very small, intense contributions to the Reynolds stress occur with a scale of the order of the viscous length. In the other investigation a pair of single hot-wires which were of a length of the order of one half the viscous length (50 Microns) were used to demonstrate the existence of shear layers near the wall with an intensity comparable to the mean shear stress at the wall. One primary results is when large scale turbulence is present in the flow upstream of the cylinder, large amplitude, low frequency circumferentially averaged pressure fluctuations are caused by pressure fluctuations in the free stream turbulence and by the aerodynamic interaction of cylinder with the free stream turbulence. A three-sensor hot-wire probe was used to measure the three components of the velocity fluctuations in the free stream at a point 3.5 diameters from the axis of the cylinder. When the free stream turbulence level was low, the instantaneous average of the pressure fluctuations around the circumference could be estimated from the free stream velocity fluctuations near the measuring point on the cylinder.
Experimental Investigation of Turbulent Flow Field and Pressure Fluctuations on Flat Surfaces and Cylinders
Author: William W. Willmarth
Publisher:
ISBN:
Category :
Languages : en
Pages : 23
Book Description
The structure of the fluctuating flow field in a turbulent boundary layer has been investigated with the aid of extremely small hot wire probes. Two investigations were conducted. In one investigations of a small X array hot-wire probe, with dimensions (length and spacing) of the order of 2.5 viscous lengths (100 Microns) was constructed and used to measure the small scale structure of the velocity fluctuations and the Reynolds stress near the wall. It was found that very small, intense contributions to the Reynolds stress occur with a scale of the order of the viscous length. In the other investigation a pair of single hot-wires which were of a length of the order of one half the viscous length (50 Microns) were used to demonstrate the existence of shear layers near the wall with an intensity comparable to the mean shear stress at the wall. One primary results is when large scale turbulence is present in the flow upstream of the cylinder, large amplitude, low frequency circumferentially averaged pressure fluctuations are caused by pressure fluctuations in the free stream turbulence and by the aerodynamic interaction of cylinder with the free stream turbulence. A three-sensor hot-wire probe was used to measure the three components of the velocity fluctuations in the free stream at a point 3.5 diameters from the axis of the cylinder. When the free stream turbulence level was low, the instantaneous average of the pressure fluctuations around the circumference could be estimated from the free stream velocity fluctuations near the measuring point on the cylinder.
Publisher:
ISBN:
Category :
Languages : en
Pages : 23
Book Description
The structure of the fluctuating flow field in a turbulent boundary layer has been investigated with the aid of extremely small hot wire probes. Two investigations were conducted. In one investigations of a small X array hot-wire probe, with dimensions (length and spacing) of the order of 2.5 viscous lengths (100 Microns) was constructed and used to measure the small scale structure of the velocity fluctuations and the Reynolds stress near the wall. It was found that very small, intense contributions to the Reynolds stress occur with a scale of the order of the viscous length. In the other investigation a pair of single hot-wires which were of a length of the order of one half the viscous length (50 Microns) were used to demonstrate the existence of shear layers near the wall with an intensity comparable to the mean shear stress at the wall. One primary results is when large scale turbulence is present in the flow upstream of the cylinder, large amplitude, low frequency circumferentially averaged pressure fluctuations are caused by pressure fluctuations in the free stream turbulence and by the aerodynamic interaction of cylinder with the free stream turbulence. A three-sensor hot-wire probe was used to measure the three components of the velocity fluctuations in the free stream at a point 3.5 diameters from the axis of the cylinder. When the free stream turbulence level was low, the instantaneous average of the pressure fluctuations around the circumference could be estimated from the free stream velocity fluctuations near the measuring point on the cylinder.
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 892
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 892
Book Description
An Experimental Investigation of Velocity Field and Wall Pressure Fluctuations in Turbulent Flows
Author: Hassan M. S. Helal
Publisher:
ISBN:
Category : Wall pressure (Aerodynamics)
Languages : en
Pages : 408
Book Description
Publisher:
ISBN:
Category : Wall pressure (Aerodynamics)
Languages : en
Pages : 408
Book Description
Experimental Investigation of Turbulent Flow in a Cylinder-flat Plate Junction Configuration with an Upstream Circular Manipulator
Author: Alan Dow
Publisher:
ISBN:
Category : Turbulence
Languages : en
Pages : 150
Book Description
Publisher:
ISBN:
Category : Turbulence
Languages : en
Pages : 150
Book Description
Technical Reports Awareness Circular : TRAC.
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 520
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 520
Book Description
Experimental Investigation of Turbulent Flow in a Rotating Cylinder During Spindown to Rest
Author: M. Mahboob Alam
Publisher:
ISBN:
Category :
Languages : en
Pages : 138
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 138
Book Description
An Experimental Investigation of Organized Turbulent Motions and Wall-pressure Fluctuations in Complex Flows
Author: Mark E. Kammeyer
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 314
Book Description
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 314
Book Description
An Experimental Investigation of Pressure Fluctuations in Three-Dimensional Turbulent Boundary Layers
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Experimental surface pressure fluctuations measurements over a wide range of Reynolds number (1400
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Experimental surface pressure fluctuations measurements over a wide range of Reynolds number (1400
Handbook of Engineering Acoustics
Author: Gerhard Müller
Publisher: Springer Science & Business Media
ISBN: 3540694609
Category : Science
Languages : en
Pages : 704
Book Description
This acoustics handbook for mechanical and architectural applications is a translation of the German standard work on the subject. It not only describes the state of art of engineering acoustics but also gives practical help to engineers for solving acoustic problems. It deals with the origin, the transmission and the methods of abatement of air-borne and structure-borne sound of different kinds, from traffic to machinery and flow induced sound.
Publisher: Springer Science & Business Media
ISBN: 3540694609
Category : Science
Languages : en
Pages : 704
Book Description
This acoustics handbook for mechanical and architectural applications is a translation of the German standard work on the subject. It not only describes the state of art of engineering acoustics but also gives practical help to engineers for solving acoustic problems. It deals with the origin, the transmission and the methods of abatement of air-borne and structure-borne sound of different kinds, from traffic to machinery and flow induced sound.
Technical Abstract Bulletin
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 912
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 912
Book Description