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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
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MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
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naca-rm-e9k25

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National Advisory Committee for Aeronautics, Research Memorandum - Study of Flow Conditions and Deflection Angle at Exit of Two Dimensional Cascade of Turbine Rotor Blades at Critical and Supercritical Pressure Ratios

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naca-rm-e9k25

  • Version
  • 85 Downloads
  • 2.14 MB File Size
  • 1 File Count
  • May 19, 2017 Create Date
  • May 19, 2017 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Research Memorandum - Study of Flow Conditions and Deflection Angle at Exit of Two Dimensional Cascade of Turbine Rotor Blades at Critical and Supercritical Pressure Ratios

FileAction
naca-rm-e9k25 Study of Flow Conditions and Deflection Angle at Exit of Two Dimensional Cascade of Turbine Rotor Blades at Critical and Supercritical Pressure Ratios.pdfDownload 
17,005 Documents in our Technical Library
2463281 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 ...