Investigation of the I-40 Jet-Propulsion Engine in the Cleveland Altitude Wind Tunnel PDF Download
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Author: Richard L. Golladay
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 76
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Author: Richard L. Golladay
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 76
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Book Description
Author: Reece V. Hensley
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 40
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Author: Richard P. Krebs
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 34
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Author: Richard L. Golladay
Publisher:
ISBN:
Category :
Languages : en
Pages : 71
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Author: Richard P. Krebs
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Author: Stanley L. Gendler
Publisher:
ISBN:
Category :
Languages : en
Pages : 75
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Author: Reece V. Hensley
Publisher:
ISBN:
Category :
Languages : en
Pages : 34
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 35
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Book Description
Performance characteristics of the centrifugal compressor of the General Electric I-40 jet-propulsion engine were determined with the engine installed in the YP-80A airplane in the Cleveland altitude wind tunnel. A standard I-40 jet-propulsion engine was used in the investigation, which was conducted over a range of simulated altitudes from 10,000 to 40,000 feet and ram-pressure ratios from 0.98 to 1.76. During the investigation the compressor Mach number varied from 0.72 to 1.46. Performance characteristics are presented as functions of corrected air flow and compressor Mach number.
Author: Robert O. Jr Dietz
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 568
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