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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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naca-rm-l54i03

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  • August 19, 2017 Create Date
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National Advisory Committee for Aeronautics, Research Memorandum - An Investigation of the Characteristics of the NACA RM-10 (With and Without Fins) in the Langley 11 Inch Hypersonic Tunnel at a Mach Number of 6.9

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naca-rm-l54i03

  • Version
  • 107 Downloads
  • 2.10 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 - An Investigation of the Characteristics of the NACA RM-10 (With and Without Fins) in the Langley 11 Inch Hypersonic Tunnel at a Mach Number of 6.9

FileAction
naca-rm-l54i03 An Investigation of the Characteristics of the NACA RM-10 (With and Without Fins) in the Langley 11 Inch Hypersonic Tunnel at a Mach Number of 6.9.pdfDownload 
17,005 Documents in our Technical Library
2464178 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 ...