Author: Charles M. Mehalic
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 46
Book Description
Steady-state Inlet Temperature Distortion Effects on the Stall Limits of a J85-GE-13 Turbojet Engine
Author: Charles M. Mehalic
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 46
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 46
Book Description
Steady-state Inlet Temperature Distorsion Effects on the Stall Limits of a J85-GE-13 Turbojet Engine
Author: Etats-Unis. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages : 37
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 37
Book Description
Steady-state Inlet Temperature Distortion Effects on the Stall Limits of a J85-GE-13 Turbojet Engine
Author: Charles M. Mehalic
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
Book Description
NASA Technical Memorandum
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 356
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 356
Book Description
Effects of Steady-State Pressure Distortion on the Stall Margin of a J85-21 Turbojet Engine
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724301253
Category :
Languages : en
Pages : 30
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
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724301253
Category :
Languages : en
Pages : 30
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
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 990
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.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 990
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
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 320
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 320
Book Description
Inventory of Energy Research and Development, 1973-1975
Author: Oak Ridge National Laboratory
Publisher:
ISBN:
Category : Power resources
Languages : en
Pages : 1356
Book Description
Publisher:
ISBN:
Category : Power resources
Languages : en
Pages : 1356
Book Description
Steady-state Interactions from Mach 1.98 to 2.58 Between a Turbojet Engine and an Axisymmetric Inlet with 60-percent Internal Area Contraction
Author: David A. Choby
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description