Author: Ralph T. Dittrich
Publisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 56
Book Description
Experimental discharge coefficients for various types of combustor-liner air-entry holes are presented as a function of a dimensionless flow parameter. In general, scoops and step louvers have higher discharge coefficients and wider flow ranges than flush holes. The effects of size or shape of a given type of hole are small. The proximity of multiple flush holes or the wall inclination of a convergent duct has a negligible effect on discharge coefficient.
Discharge Coefficients for Combustor-liner Air-entry Holes
Author: Ralph T. Dittrich
Publisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 56
Book Description
Experimental discharge coefficients for various types of combustor-liner air-entry holes are presented as a function of a dimensionless flow parameter. In general, scoops and step louvers have higher discharge coefficients and wider flow ranges than flush holes. The effects of size or shape of a given type of hole are small. The proximity of multiple flush holes or the wall inclination of a convergent duct has a negligible effect on discharge coefficient.
Publisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 56
Book Description
Experimental discharge coefficients for various types of combustor-liner air-entry holes are presented as a function of a dimensionless flow parameter. In general, scoops and step louvers have higher discharge coefficients and wider flow ranges than flush holes. The effects of size or shape of a given type of hole are small. The proximity of multiple flush holes or the wall inclination of a convergent duct has a negligible effect on discharge coefficient.
Discharge Coefficients for Combustor-liner Air-entry Holes
Author: Ralph T. Dittrich
Publisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 690
Book Description
An experimental investigation was conducted to determine the effects of various geometric and flow factors on the discharge coefficients for circular holes having flow parallel to the plane of the hole. The geometric and flow factors considered were hole diameter, wall thickness at the hole, parallel-fllow duct height, boundary-layer thickness, parallel-flow velocity, static-pressure level, and pressure ratio across the test hole.
Publisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 690
Book Description
An experimental investigation was conducted to determine the effects of various geometric and flow factors on the discharge coefficients for circular holes having flow parallel to the plane of the hole. The geometric and flow factors considered were hole diameter, wall thickness at the hole, parallel-fllow duct height, boundary-layer thickness, parallel-flow velocity, static-pressure level, and pressure ratio across the test hole.
Discharge Coefficients for Combustor-liner Air-entry Holes
Author: Ralph T. Dittrich
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Discharge Coefficient and Jet Deflection Studies for Combustor Liner Air - Entry Holes
Author: K. Sh Kaddah
Publisher:
ISBN:
Category :
Languages : en
Pages : 600
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 600
Book Description
Circular Holes with Parallel Flow
Author: Charles C. Graves
Publisher:
ISBN:
Category :
Languages : en
Pages : 39
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 39
Book Description
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1016
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1016
Book Description
Discharge Coefficients for Cumbustor-linear Air Entry Holes I - Circular Holes with Parallel Flow
Author: Ralph T. Dittrich
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 39
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 39
Book Description
Flow Coefficients and Jet Deflection Angles for Combustor-liner Entry Holes
Author: W. F. Venneman
Publisher:
ISBN:
Category :
Languages : en
Pages : 16
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 16
Book Description
Discharge Coefficients for Thick Plate Orifices with Approach Flow Perpendicular and Inclined to the Orifice Axis
Author: John E. Rohde
Publisher:
ISBN:
Category : Nozzles
Languages : en
Pages : 36
Book Description
Discharge nozzle coefficients for thick plate orifices with approach flow perpendicular and inclined to orifice axis.
Publisher:
ISBN:
Category : Nozzles
Languages : en
Pages : 36
Book Description
Discharge nozzle coefficients for thick plate orifices with approach flow perpendicular and inclined to orifice axis.
GAS Turbine Combustion, Second Edition
Author: Arthur H. Lefebvre
Publisher: CRC Press
ISBN: 9781560326731
Category : Technology & Engineering
Languages : en
Pages : 420
Book Description
This revised edition provides understanding of the basic physical, chemical, and aerodynamic processes associated with gas turbine combustion and their relevance and application to combustor performance and design. It also introduces the many new concepts for ultra-low emissions combustors, and new advances in fuel preparation and liner wall-cooling techniques for their success. It details advanced and practical approaches to combustor design for the clean burning of alternative liquid fuels derived from oil shades, tar sands, and coal. Additional topics include diffusers, combustion performance fuel injection, combustion noise, heat transfer, and emissions.
Publisher: CRC Press
ISBN: 9781560326731
Category : Technology & Engineering
Languages : en
Pages : 420
Book Description
This revised edition provides understanding of the basic physical, chemical, and aerodynamic processes associated with gas turbine combustion and their relevance and application to combustor performance and design. It also introduces the many new concepts for ultra-low emissions combustors, and new advances in fuel preparation and liner wall-cooling techniques for their success. It details advanced and practical approaches to combustor design for the clean burning of alternative liquid fuels derived from oil shades, tar sands, and coal. Additional topics include diffusers, combustion performance fuel injection, combustion noise, heat transfer, and emissions.