Author: Ashwani K. Gupta
Publisher: Taylor & Francis
ISBN: 9780856263286
Category : Crafts & Hobbies
Languages : en
Pages : 426
Book Description
First published in 2004. Routledge is an imprint of Taylor & Francis, an informa company.
Flowfield Modeling and Diagnostics
Author: Ashwani K. Gupta
Publisher: Taylor & Francis
ISBN: 9780856263286
Category : Crafts & Hobbies
Languages : en
Pages : 426
Book Description
First published in 2004. Routledge is an imprint of Taylor & Francis, an informa company.
Publisher: Taylor & Francis
ISBN: 9780856263286
Category : Crafts & Hobbies
Languages : en
Pages : 426
Book Description
First published in 2004. Routledge is an imprint of Taylor & Francis, an informa company.
Flow Field Diagnostics in the Compressor Research Facility One-tenth Scale Flow Model
Author: Tsuyoshi Shinji (CAPT, JASDF.)
Publisher:
ISBN:
Category : Compressors
Languages : en
Pages : 220
Book Description
Publisher:
ISBN:
Category : Compressors
Languages : en
Pages : 220
Book Description
Laser Diagnostic Development and Measurement and Modeling of Turbulent Flowfields of Jets and Wakes
Flow Field Diagnostics in the Compressor Research Facility One-Tenth Scale Flow Model
Author: Tsuyoshi Shinji
Publisher:
ISBN:
Category :
Languages : en
Pages : 128
Book Description
The Air Force Aero Propulsion Laboratory is developing a compressor research facility (CRF). The facility must provide a metered flow at a given pressure which is uniform in temperature and velocity at the compressor inlet. In this study the flow field of a one-tenth scale flow model of the CRF, constructed by a contractor for the Air Force Aero Propulsion Laboratory, was investigated. Velocity measurements made with a constant temperature anemometer using hot wire sensors provided the basis for establishing velocity profiles and turbulence intensity levels.
Publisher:
ISBN:
Category :
Languages : en
Pages : 128
Book Description
The Air Force Aero Propulsion Laboratory is developing a compressor research facility (CRF). The facility must provide a metered flow at a given pressure which is uniform in temperature and velocity at the compressor inlet. In this study the flow field of a one-tenth scale flow model of the CRF, constructed by a contractor for the Air Force Aero Propulsion Laboratory, was investigated. Velocity measurements made with a constant temperature anemometer using hot wire sensors provided the basis for establishing velocity profiles and turbulence intensity levels.
Laser Diagnostic Development and Measurement and Modeling of Turbulent Flowfields of Jets and Wakes
Author: S. O. Park
Publisher:
ISBN:
Category : Gas flow
Languages : en
Pages : 121
Book Description
Finite-difference numerical computations are presented to predict the isothermal, turbulent, recirculating flowfields in a centerbody combustor configuration which involves confined dual coaxial jet mixing in the near-wake region of an axisymmetric bluff body. Calculations based upon the Reynolds-averaged Navier-Stokes equations and the k-epsilon turbulence model consider the influence of the annular and central flow rates on the nature of the flowfield downstream of the bluff body. The reported isothermal modeling calculations are performed with the 'Teaching Elliptic Axisymmetrical Characteristics Heuristically' (TEACH) Code. Numerical results show the influence of the annular and central jet flow rates on the distributions of the mean and rms velocity fields and centerline locations of stagnation points. The sensitivity of the predicted results to several aspects of the modeling is considered. The predicted results demonstrate the complexity of flowfield interactions in the near-wake region and refine the understanding of the centerbody combustor flowfields. The character of the recirculating flowfield emerging from the numerical predictions when the near-wake is dominated by the annular jet is in conformity with experimental observations.
Publisher:
ISBN:
Category : Gas flow
Languages : en
Pages : 121
Book Description
Finite-difference numerical computations are presented to predict the isothermal, turbulent, recirculating flowfields in a centerbody combustor configuration which involves confined dual coaxial jet mixing in the near-wake region of an axisymmetric bluff body. Calculations based upon the Reynolds-averaged Navier-Stokes equations and the k-epsilon turbulence model consider the influence of the annular and central flow rates on the nature of the flowfield downstream of the bluff body. The reported isothermal modeling calculations are performed with the 'Teaching Elliptic Axisymmetrical Characteristics Heuristically' (TEACH) Code. Numerical results show the influence of the annular and central jet flow rates on the distributions of the mean and rms velocity fields and centerline locations of stagnation points. The sensitivity of the predicted results to several aspects of the modeling is considered. The predicted results demonstrate the complexity of flowfield interactions in the near-wake region and refine the understanding of the centerbody combustor flowfields. The character of the recirculating flowfield emerging from the numerical predictions when the near-wake is dominated by the annular jet is in conformity with experimental observations.
EPA's Rule on Paints and Coatings
Author: United States. Congress. House. Committee on Science. Subcommittee on Energy and Environment
Publisher:
ISBN:
Category : Law
Languages : en
Pages : 910
Book Description
Publisher:
ISBN:
Category : Law
Languages : en
Pages : 910
Book Description
NOAA Professional Paper
Laser Diagnostic Development and Measurement and Modeling of Turbulent Flowfields of Jets and Wakes
Author: L. Krishnamurthy
Publisher:
ISBN:
Category : Gas flow
Languages : en
Pages : 135
Book Description
Finite-difference numerical computations are presented to predict the isothermal, turbulent, recirculating flowfields in a centerbody combustor configuration which involves confined dual coaxial jet mixing in the near-wake region of an axisymmetric bluff body. Calculations based upon the Reynolds-averaged Navier-Stokes equations and the k-epsilon turbulence model consider the influence of the annular and central flow rates on the nature of the flowfield downstream of the bluff body. The reported isothermal modeling calculations are performed with the 'Teaching Elliptic Axisymmetrical Characteristics Heuristically' (TEACH) Code. Numerical results show the influence of the annular and central jet flow rates on the distributions of the mean and rms velocity fields and centerline locations of stagnation points. The sensitivity of the predicted results to several aspects of the modeling is considered. The predicted results demonstrate the complexity of flowfield interactions in the near-wake region and refine the understanding of the centerbody combustor flowfields. The character of the recirculating flowfield emerging from the numerical predictions when the near-wake is dominated by the annular jet is in conformity with experimental observations.
Publisher:
ISBN:
Category : Gas flow
Languages : en
Pages : 135
Book Description
Finite-difference numerical computations are presented to predict the isothermal, turbulent, recirculating flowfields in a centerbody combustor configuration which involves confined dual coaxial jet mixing in the near-wake region of an axisymmetric bluff body. Calculations based upon the Reynolds-averaged Navier-Stokes equations and the k-epsilon turbulence model consider the influence of the annular and central flow rates on the nature of the flowfield downstream of the bluff body. The reported isothermal modeling calculations are performed with the 'Teaching Elliptic Axisymmetrical Characteristics Heuristically' (TEACH) Code. Numerical results show the influence of the annular and central jet flow rates on the distributions of the mean and rms velocity fields and centerline locations of stagnation points. The sensitivity of the predicted results to several aspects of the modeling is considered. The predicted results demonstrate the complexity of flowfield interactions in the near-wake region and refine the understanding of the centerbody combustor flowfields. The character of the recirculating flowfield emerging from the numerical predictions when the near-wake is dominated by the annular jet is in conformity with experimental observations.
Advanced and Intelligent Computations in Diagnosis and Control
Author: Zdzisław Kowalczuk
Publisher: Springer
ISBN: 3319231804
Category : Technology & Engineering
Languages : en
Pages : 417
Book Description
This book is devoted to the demands of research and industrial centers for diagnostics, monitoring and decision making systems that result from the increasing complexity of automation and systems, the need to ensure the highest level of reliability and safety, and continuing research and the development of innovative approaches to fault diagnosis. The contributions combine domains of engineering knowledge for diagnosis, including detection, isolation, localization, identification, reconfiguration and fault-tolerant control. The book is divided into six parts: (I) Fault Detection and Isolation; (II) Estimation and Identification; (III) Robust and Fault Tolerant Control; (IV) Industrial and Medical Diagnostics; (V) Artificial Intelligence; (VI) Expert and Computer Systems.
Publisher: Springer
ISBN: 3319231804
Category : Technology & Engineering
Languages : en
Pages : 417
Book Description
This book is devoted to the demands of research and industrial centers for diagnostics, monitoring and decision making systems that result from the increasing complexity of automation and systems, the need to ensure the highest level of reliability and safety, and continuing research and the development of innovative approaches to fault diagnosis. The contributions combine domains of engineering knowledge for diagnosis, including detection, isolation, localization, identification, reconfiguration and fault-tolerant control. The book is divided into six parts: (I) Fault Detection and Isolation; (II) Estimation and Identification; (III) Robust and Fault Tolerant Control; (IV) Industrial and Medical Diagnostics; (V) Artificial Intelligence; (VI) Expert and Computer Systems.