Effects of Steady-State Pressure Distortion on the Stall Margin of a J85-21 Turbojet Engine

Effects of Steady-State Pressure Distortion on the Stall Margin of a J85-21 Turbojet Engine PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724301253
Category :
Languages : en
Pages : 30

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Book Description
The effects of the inlet pressure distortions, induced by five screen patterns, on the performance of a J85-21 turbojet engine was conducted at the NASA Lewis Research Center. Testing was in support of the HiMAT RPRV program at Dryden Flight Research Center. Distortion patterns were chosen based on anticipated application of test results of the HiMAT installation. Tests were conducted at a simulated Mach number and altitude condition of 0.9 and 10 973 meters. Results are presented in terms of distortion levels and standard compressor performance parameters. Bobula, G. A. Glenn Research Center NASA-TM-79123, E-9958, AVRADCOM-TR-79-12

Effects of Steady-State Pressure Distortion on the Stall Margin of a J85-21 Turbojet Engine

Effects of Steady-State Pressure Distortion on the Stall Margin of a J85-21 Turbojet Engine PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724301253
Category :
Languages : en
Pages : 30

Get Book Here

Book Description
The effects of the inlet pressure distortions, induced by five screen patterns, on the performance of a J85-21 turbojet engine was conducted at the NASA Lewis Research Center. Testing was in support of the HiMAT RPRV program at Dryden Flight Research Center. Distortion patterns were chosen based on anticipated application of test results of the HiMAT installation. Tests were conducted at a simulated Mach number and altitude condition of 0.9 and 10 973 meters. Results are presented in terms of distortion levels and standard compressor performance parameters. Bobula, G. A. Glenn Research Center NASA-TM-79123, E-9958, AVRADCOM-TR-79-12

Effects of Steady-state Pressure Distortion on the Stall Margin of a J85-21 Turbojet Engine

Effects of Steady-state Pressure Distortion on the Stall Margin of a J85-21 Turbojet Engine PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 32

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Steady-state Inlet Temperature Distortion Effects on the Stall Limits of a J85-GE-13 Turbojet Engine

Steady-state Inlet Temperature Distortion Effects on the Stall Limits of a J85-GE-13 Turbojet Engine PDF Author: Charles M. Mehalic
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 990

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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 932

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Steady-state Performance of J85-21 Compressor at 100 Percent of Design Speed with and Without Interstage Rake Blockage

Steady-state Performance of J85-21 Compressor at 100 Percent of Design Speed with and Without Interstage Rake Blockage PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 40

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Experimental Investigation of the Effect of Screen Induced Total Pressure Distortion on Turbojet Stall Margin

Experimental Investigation of the Effect of Screen Induced Total Pressure Distortion on Turbojet Stall Margin PDF Author: Paul L. Burstadt
Publisher:
ISBN:
Category :
Languages : en
Pages : 60

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NASA Scientific and Technical Reports

NASA Scientific and Technical Reports PDF Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966

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Steady-state Inlet Temperature Distorsion Effects on the Stall Limits of a J85-GE-13 Turbojet Engine

Steady-state Inlet Temperature Distorsion Effects on the Stall Limits of a J85-GE-13 Turbojet Engine PDF Author: Etats-Unis. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages : 37

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NASA SP.

NASA SP. PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 520

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