17,005 Documents in our Technical Library
2727313 Total Downloads

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 ...

ARC-RM-3209

ARC-RM-3209
  • Version
  • 169 Downloads
  • 3.79 MB File Size
  • 1 File Count
  • June 28, 2016 Create Date
  • June 28, 2016 Last Updated
Scroll for Details

An Experimental Investigation of the Transonic Flow over an Unswept Wing of Aspect Ratio 3.5, Taper Ratio 0.5, with a 4% Biconvex Section

ARC-RM-3209 An Experimental Investigation of the Transonic Flow over an Unswept Wing of Aspect Ratio 3.5, Taper Ratio 0.5, with a 4% Biconvex Section

FileAction
ARC-RM-3209 An Experimental Investigation of the Transonic Flow over an Unswept Wing of Aspect Ratio 3.5, Taper Ratio 0.5, with a 4% Biconvex Section.pdfDownload 

Comment On This Post

Your email address will not be published. Required fields are marked *

ARC-RM-3209

ARC-RM-3209
  • Version
  • 169 Downloads
  • 3.79 MB File Size
  • 1 File Count
  • June 28, 2016 Create Date
  • June 28, 2016 Last Updated
Scroll for Details

An Experimental Investigation of the Transonic Flow over an Unswept Wing of Aspect Ratio 3.5, Taper Ratio 0.5, with a 4% Biconvex Section

ARC-RM-3209 An Experimental Investigation of the Transonic Flow over an Unswept Wing of Aspect Ratio 3.5, Taper Ratio 0.5, with a 4% Biconvex Section

FileAction
ARC-RM-3209 An Experimental Investigation of the Transonic Flow over an Unswept Wing of Aspect Ratio 3.5, Taper Ratio 0.5, with a 4% Biconvex Section.pdfDownload 
17,005 Documents in our Technical Library
2727313 Total Downloads

Search The Technical Library

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 ...