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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-tn-1696

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National Advisory Committee for Aeronautics, Technical Notes - Chordwise Pressure Distributions on a 12' Span Wing of NACA 66-Series Airfoil Sections Up to a Mach Number of 0.60

naca-tn-1696-chordwise-pressure-distributions-on-a-12-span-wing-of-naca-66-series-airfoil-sections-up-to-a-mach-number-of-0-60-1

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naca-tn-1696

  • Version
  • 0 Downloads
  • 0.00 KB File Size
  • 0 File Count
  • December 6, 2016 Create Date
  • December 6, 2016 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Technical Notes - Chordwise Pressure Distributions on a 12' Span Wing of NACA 66-Series Airfoil Sections Up to a Mach Number of 0.60

naca-tn-1696-chordwise-pressure-distributions-on-a-12-span-wing-of-naca-66-series-airfoil-sections-up-to-a-mach-number-of-0-60-1

17,005 Documents in our Technical Library
2727309 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 ...