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NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
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ADPO10769 Occurrence of Corrosion in Airframes
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naca-tn-1050

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National Advisory Committee for Aeronautics, Technical Notes - Wind Tunnel Investigations of End Plate Effects of Horizontal Tails on a Vertical Tail Compared with Available Theory

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naca-tn-1050

  • Version
  • 152 Downloads
  • 1.32 MB File Size
  • 1 File Count
  • December 2, 2016 Create Date
  • December 2, 2016 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Technical Notes - Wind Tunnel Investigations of End Plate Effects of Horizontal Tails on a Vertical Tail Compared with Available Theory

naca-tn-1050-wind-tunnel-investigations-of-end-plate-effects-of-horizontal-tails-on-a-vertical-tail-compared-with-available-theory-1

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naca-tn-1050 Wind Tunnel Investigations of End Plate Effects of Horizontal Tails on a Vertical Tail Compared with Available Theory.pdfDownload 
17,005 Documents in our Technical Library
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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 ...