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ADPO10769 Occurrence of Corrosion in Airframes
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naca-report-1208

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National Advisory Committee for Aeronautics, Report - A Comparison of the Spanwise Loading Calculated by Various Methods with Experimental Loadings Obtained on a 45° Sweptback Wing of Aspect Ratio 8.02 at Reynolds Number of 4.0 x 10

naca-report-1208-a-comparison-of-the-spanwise-loading-calculated-by-various-methods-with-experimental-loadings-obtained-ona-45-sweptback-wing-of-aspect-ratio-8-02-at-reynolds-1

 

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naca-report-1208

  • Version
  • 210 Downloads
  • 1.27 MB File Size
  • 1 File Count
  • November 2, 2016 Create Date
  • November 2, 2016 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Report - A Comparison of the Spanwise Loading Calculated by Various Methods with Experimental Loadings Obtained on a 45° Sweptback Wing of Aspect Ratio 8.02 at Reynolds Number of 4.0 x 10

naca-report-1208-a-comparison-of-the-spanwise-loading-calculated-by-various-methods-with-experimental-loadings-obtained-ona-45-sweptback-wing-of-aspect-ratio-8-02-at-reynolds-1

 

FileAction
naca-report-1208 A Comparison of the Spanwise Loading Calculated by Various Methods with Experimental Loadings Obtained on a 45° Sweptback Wing of Aspect Ratio 8.02 at Reynolds.pdfDownload 
17,005 Documents in our Technical Library
2727452 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 ...