Effect of Combustor-inlet Conditions on Performance of an Annular Turbojet Combustor

Effect of Combustor-inlet Conditions on Performance of an Annular Turbojet Combustor PDF Author: J. Howard Childs
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 56

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Book Description
The combustion performance and particularly the phenomenon of altitude operational limits was studied by operating the annular combustor of a turbojet engine over a range of conditions of air flow, inlet pressure, inlet temperature, and fuel flow. The combustor investigated was not the latest version of this combustor and the data are presented primarily because they are indicative of general trends and phenomena that apply to a large class of turbojet combustors.

Effect of Combustor-inlet Conditions on Performance of an Annular Turbojet Combustor

Effect of Combustor-inlet Conditions on Performance of an Annular Turbojet Combustor PDF Author: J. Howard Childs
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 56

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Book Description
The combustion performance and particularly the phenomenon of altitude operational limits was studied by operating the annular combustor of a turbojet engine over a range of conditions of air flow, inlet pressure, inlet temperature, and fuel flow. The combustor investigated was not the latest version of this combustor and the data are presented primarily because they are indicative of general trends and phenomena that apply to a large class of turbojet combustors.

Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 816

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Report

Report PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 24

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Technical Note

Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 602

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Performance Investigation of Can-type Combustor from British Turbojet Engine and Comparison of this Combustor with Can-type Combustor from U.S. Turbojet Engine

Performance Investigation of Can-type Combustor from British Turbojet Engine and Comparison of this Combustor with Can-type Combustor from U.S. Turbojet Engine PDF Author: William P. Cook
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 30

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Annual Report - National Advisory Committee for Aeronautics

Annual Report - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :

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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

Report - National Advisory Committee for Aeronautics

Report - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 516

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Report

Report PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1138

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NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 814

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Vapor-fuel-distribution Effects on Combustion Performance of a Single Tubular Combustor

Vapor-fuel-distribution Effects on Combustion Performance of a Single Tubular Combustor PDF Author: Richard J. McCafferty
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32

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