17,005 Documents in our Technical Library
2727314 Total Downloads

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 ...

ARC-RM-2928

ARC-RM-2928
  • Version
  • 222 Downloads
  • 1.89 MB File Size
  • 1 File Count
  • June 24, 2016 Create Date
  • June 24, 2016 Last Updated
Scroll for Details

A Detailed Experimental Comparison of Axial Compressor Blades Designed for Free Vortex Flow and Equivalent Untwisted and Twisted Constant Section Blades

ARC-RM-2928 A Detailed Experimental Comparison of Axial Compressor Blades Designed for Free Vortex Flow and Equivalent Untwisted and Twisted Constant Section Blades

FileAction
ARC-RM-2928 A Detailed Experimental Comparison of Axial Compressor Blades Designed for Free Vortex Flow and Equivalent Untwisted and Twisted Constant Section Blades.pdfDownload 

Comment On This Post

Your email address will not be published. Required fields are marked *

ARC-RM-2928

ARC-RM-2928
  • Version
  • 222 Downloads
  • 1.89 MB File Size
  • 1 File Count
  • June 24, 2016 Create Date
  • June 24, 2016 Last Updated
Scroll for Details

A Detailed Experimental Comparison of Axial Compressor Blades Designed for Free Vortex Flow and Equivalent Untwisted and Twisted Constant Section Blades

ARC-RM-2928 A Detailed Experimental Comparison of Axial Compressor Blades Designed for Free Vortex Flow and Equivalent Untwisted and Twisted Constant Section Blades

FileAction
ARC-RM-2928 A Detailed Experimental Comparison of Axial Compressor Blades Designed for Free Vortex Flow and Equivalent Untwisted and Twisted Constant Section Blades.pdfDownload 
17,005 Documents in our Technical Library
2727314 Total Downloads

Search The Technical Library

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 ...