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NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
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AA-CP-20212-001
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ADPO10769 Occurrence of Corrosion in Airframes
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MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
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naca-report-1245

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National Advisory Committee for Aeronautics, Report - Analysis and Calculation by Integral Methods of Laminar Compressible Boundary Layer with Heat Transfer and with and Without Pressure Gradient

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naca-report-1245

  • Version
  • 176 Downloads
  • 2.65 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 - Analysis and Calculation by Integral Methods of Laminar Compressible Boundary Layer with Heat Transfer and with and Without Pressure Gradient

naca-report-1245-analysis-and-calculation-by-integral-methods-of-laminar-compressible-boundary-layer-with-heat-transfer-and-with-and-without-pressure-gradient-1

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naca-report-1245 Analysis and Calculation by Integral Methods of Laminar Compressible Boundary Layer with Heat Transfer and with and Without Pressure Gradient.pdfDownload 
17,005 Documents in our Technical Library
2727440 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 ...