Performance Of Naca Eight Stage Axial Flow Compressor Designed On The Basis Of Airfoil Theory

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Performance of NACA Eight-stage Axial-flow Compressor Designed on the Basis of Airfoil Theory

Author : John T. Sinnette,Oscar W. Schey,J. Austin King
Publisher : Unknown
Page : 74 pages
File Size : 53,5 Mb
Release : 1944
Category : Aerofoils
ISBN : UOM:39015095014299

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Performance of NACA Eight-stage Axial-flow Compressor Designed on the Basis of Airfoil Theory by John T. Sinnette,Oscar W. Schey,J. Austin King Pdf

The NACA has conducted an investigation to determine the performance that can be obtained from a multistage axial-flow compressor based on airfoil research. A theory was developed; an eight-stage axial-flow compressor was designed, constructed, and tested.

Performance of NACA Eight-stage Axial-flow Compressor at Simulated Altitude

Author : J. Austin King,Owen W. Regan
Publisher : Unknown
Page : 30 pages
File Size : 42,8 Mb
Release : 1944
Category : Axial flow compressors
ISBN : UOM:39015095014331

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Performance of NACA Eight-stage Axial-flow Compressor at Simulated Altitude by J. Austin King,Owen W. Regan Pdf

An investigation has been conducted by the NACA to determine the design-performance characteristics of the NACA eight-stage axial-flow compressor and the effect of altitude on the performance. The compressor was tested at simulated altitudes of 50,000; 36,000; and 27,000 feet at rotor speeds corresponding to compressor Mach numbers of 0.80, 0.85, 0.90, and 0.95 wit varying air flow at each speed.

NACA Research Memorandum

Author : Anonim
Publisher : Unknown
Page : 488 pages
File Size : 44,9 Mb
Release : 1958
Category : Aerodynamics
ISBN : STANFORD:36105024809746

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NACA Research Memorandum by Anonim Pdf

Annual Report of the National Advisory Committee for Aeronautics

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 664 pages
File Size : 44,8 Mb
Release : 1951
Category : Aeronautics
ISBN : OSU:32435025576174

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Annual Report of the National Advisory Committee for Aeronautics by United States. National Advisory Committee for Aeronautics Pdf

Report

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 36 pages
File Size : 41,7 Mb
Release : 1950
Category : Aeronautics
ISBN : STANFORD:36105024788916

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Report by United States. National Advisory Committee for Aeronautics Pdf

Report - National Advisory Committee for Aeronautics

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 468 pages
File Size : 42,6 Mb
Release : 1943
Category : Aeronautics
ISBN : CORNELL:31924089862308

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Report - National Advisory Committee for Aeronautics by United States. National Advisory Committee for Aeronautics Pdf

Aerodynamic Design of Axial Flow Compressors

Author : Robert O. Bullock
Publisher : Unknown
Page : 552 pages
File Size : 43,8 Mb
Release : 1965
Category : Axial flow compressors
ISBN : NASA:31769000652464

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Aerodynamic Design of Axial Flow Compressors by Robert O. Bullock Pdf

Aerodynamic Design of Axial-flow Compressors

Author : Lewis Research Center
Publisher : Unknown
Page : 542 pages
File Size : 55,5 Mb
Release : 1965
Category : Axial flow compressors
ISBN : STANFORD:36105113764901

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Aerodynamic Design of Axial-flow Compressors by Lewis Research Center Pdf

Index of NACA Technical Publications

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 1370 pages
File Size : 41,9 Mb
Release : 1949
Category : Aeronautics
ISBN : UFL:31262082080614

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Index of NACA Technical Publications by United States. National Advisory Committee for Aeronautics Pdf

Wartime Report

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 334 pages
File Size : 46,6 Mb
Release : 1944
Category : Aeronautics
ISBN : UOM:39015020152602

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Wartime Report by United States. National Advisory Committee for Aeronautics Pdf

Charts of Pressure Rise Obtainable with Airfoil-type Axial-flow Cooling Fans

Author : A. Kahane
Publisher : Unknown
Page : 578 pages
File Size : 55,8 Mb
Release : 1947
Category : Aerofoils
ISBN : STANFORD:36105024795291

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Charts of Pressure Rise Obtainable with Airfoil-type Axial-flow Cooling Fans by A. Kahane Pdf

Charts are presented to show the pressure rise that is obtainable in an engine-cooling installation with a typical airfoil-type propeller-speed fan. The charts cover fans of the stator-rotor, rotor-stator, and rotor alone configurations, with blades incorporating both the highly cambered 65-series blower-blade sections and the conventional low-cambered airfoil sections. The effects of operation of a geared fan with rotational speeds limited by compressibility considerations and the effects of initial rotational inflow are indicated. Use of the charts to predict the pressure rise obtainable with any fan of the types considered is illustrated in a sample calculation.

Investigation of an Impulse Axial-flow Compressor

Author : John R. Erwin,Wallace M. Schulze
Publisher : Unknown
Page : 56 pages
File Size : 55,9 Mb
Release : 1950
Category : Axial flow compressors
ISBN : UOM:39015086464552

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Investigation of an Impulse Axial-flow Compressor by John R. Erwin,Wallace M. Schulze Pdf