Altitude Performance of Annular Combustor Type Turbojet Engine with JFC-2 Fuel PDF Download

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Altitude Performance of Annular Combustor Type Turbojet Engine with JFC-2 Fuel

Altitude Performance of Annular Combustor Type Turbojet Engine with JFC-2 Fuel PDF Author: James W. Useller
Publisher:
ISBN:
Category :
Languages : en
Pages : 19

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Altitude Performance of Annular Combustor Type Turbojet Engine with JFC-2 Fuel

Altitude Performance of Annular Combustor Type Turbojet Engine with JFC-2 Fuel PDF Author: James W. Useller
Publisher:
ISBN:
Category :
Languages : en
Pages : 19

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Book Description

Performance Comparisons of JFC-2 and MIL-F-5624A (JP-3) Fuels in Tubular and Annular Combustors

Performance Comparisons of JFC-2 and MIL-F-5624A (JP-3) Fuels in Tubular and Annular Combustors PDF Author: Richard J. McCafferty
Publisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 28

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Book Description

Simulated Altitude Performance of Two Annular Combustors with Continuous Axial Openings for Admission of Primary Air

Simulated Altitude Performance of Two Annular Combustors with Continuous Axial Openings for Admission of Primary Air PDF Author: Eugene V. Zettle
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 44

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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.

Altitude Performance Investigation of Two Single-annular Type Combustors and the Prototype J40-WE-8 Turbojet Engine Combustor with Various Combustor-inlet Air Pressure Profiles

Altitude Performance Investigation of Two Single-annular Type Combustors and the Prototype J40-WE-8 Turbojet Engine Combustor with Various Combustor-inlet Air Pressure Profiles PDF Author: Adam E. Sobolewski
Publisher:
ISBN:
Category :
Languages : en
Pages : 46

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Book Description

Altitude Performance Investigation of Single- and Double-annular Turbojet-engine Combustors with Various Size Fuel Nozzles

Altitude Performance Investigation of Single- and Double-annular Turbojet-engine Combustors with Various Size Fuel Nozzles PDF Author: James L. Jr Harp
Publisher:
ISBN:
Category :
Languages : en
Pages : 60

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Book Description

Performance of Experimental Channeled-wall Annular Turbojet Combustor at Conditions Simulating High-altitude Supersonic Flight

Performance of Experimental Channeled-wall Annular Turbojet Combustor at Conditions Simulating High-altitude Supersonic Flight PDF Author: Eugene V. Zettle
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 24

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Book Description

Investigation of Altitude Performance of AN-F-58 Fuels in Annular Combustor of 34-WE-22 Engine

Investigation of Altitude Performance of AN-F-58 Fuels in Annular Combustor of 34-WE-22 Engine PDF Author: Adelbert O. Tischler
Publisher:
ISBN:
Category :
Languages : en
Pages : 35

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Investigation of Altitude Performance of AN-F-58 Fuels in Annular Combustor of J34-WE-22 Engine

Investigation of Altitude Performance of AN-F-58 Fuels in Annular Combustor of J34-WE-22 Engine PDF Author: Adelbert O. Tischler
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 35

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Book Description

High-altitude Performance of 9.5-inch-diameter Tubular Experimental Combustor with Fuel Staging

High-altitude Performance of 9.5-inch-diameter Tubular Experimental Combustor with Fuel Staging PDF Author: Wilfred E. Scull
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 64

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Book Description