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 : 46

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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 : 46

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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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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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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 356

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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:
Publisher:
ISBN:
Category :
Languages : en
Pages : 32

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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.

Engine Response to Distorted Inflow Conditions

Engine Response to Distorted Inflow Conditions PDF Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 320

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Inventory of Energy Research and Development, 1973-1975

Inventory of Energy Research and Development, 1973-1975 PDF Author: Oak Ridge National Laboratory
Publisher:
ISBN:
Category : Power resources
Languages : en
Pages : 1356

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Steady-state Interactions from Mach 1.98 to 2.58 Between a Turbojet Engine and an Axisymmetric Inlet with 60-percent Internal Area Contraction

Steady-state Interactions from Mach 1.98 to 2.58 Between a Turbojet Engine and an Axisymmetric Inlet with 60-percent Internal Area Contraction PDF Author: David A. Choby
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

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