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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-l54i09

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  • August 19, 2017 Create Date
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National Advisory Committee for Aeronautics, Research Memorandum - Effect of a Wing Leading Edge Flap and Chord Extension on the High Subsonic Control Characteristics of a Spoiler Slot Deflector Control Located at Two Spanwise Positions

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naca-rm-l54i09

  • Version
  • 101 Downloads
  • 2.81 MB File Size
  • 1 File Count
  • August 19, 2017 Create Date
  • August 19, 2017 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Research Memorandum - Effect of a Wing Leading Edge Flap and Chord Extension on the High Subsonic Control Characteristics of a Spoiler Slot Deflector Control Located at Two Spanwise Positions

FileAction
naca-rm-l54i09 Effect of a Wing Leading Edge Flap and Chord Extension on the High Subsonic Control Characteristics of a.pdfDownload 
17,005 Documents in our Technical Library
2450007 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 ...