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NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
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ARC-RM-2891

ARC-RM-2891
  • Version
  • 224 Downloads
  • 3.47 MB File Size
  • 1 File Count
  • June 24, 2016 Create Date
  • June 24, 2016 Last Updated
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An Examination of the Flow and Pressure Losses in Blade Rows of Axial Flow Turbines

ARC-RM-2891 An Examination of the Flow and Pressure Losses in Blade Rows of Axial Flow Turbines

 

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ARC-RM-2891

ARC-RM-2891
  • Version
  • 224 Downloads
  • 3.47 MB File Size
  • 1 File Count
  • June 24, 2016 Create Date
  • June 24, 2016 Last Updated
Scroll for Details

An Examination of the Flow and Pressure Losses in Blade Rows of Axial Flow Turbines

ARC-RM-2891 An Examination of the Flow and Pressure Losses in Blade Rows of Axial Flow Turbines

 

FileAction
ARC-RM-2891 An Examination of the Flow and Pressure Losses in Blade Rows of Axial Flow Turbines.pdfDownload 
17,005 Documents in our Technical Library
2727307 Total Downloads

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Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...