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
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
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
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.
Applied Mechanics Reviews
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 932
Book Description
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 932
Book Description
Steady-state Performance of J85-21 Compressor at 100 Percent of Design Speed with and Without Interstage Rake Blockage
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Book Description
Experimental Investigation of the Effect of Screen Induced Total Pressure Distortion on Turbojet Stall Margin
Author: Paul L. Burstadt
Publisher:
ISBN:
Category :
Languages : en
Pages : 60
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 60
Book Description
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966
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
NASA SP.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 520
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 520
Book Description