ARC-CP-418

ARC-CP-418
  • Version
  • 191 Downloads
  • 2.62 MB File Size
  • 1 File Count
  • July 14, 2016 Create Date
  • July 14, 2016 Last Updated
▼ Scroll for Details ▼

An Improvement of the Velocity Distribution Predicted by Linear Theory for Wings with Straight Subsonic Leading Edges

ARC-CP-418 An Improvement of the Velocity Distribution Predicted by Linear Theory for Wings with Straight Subsonic Leading Edges

FileAction
ARC-CP-418 An Improvement of the Velocity Distribution Predicted by Linear Theory for Wings with Straight Subsonic Leading Edges.pdfDownload 

Comment On This Post

Your email address will not be published.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

ARC-CP-418

ARC-CP-418
  • Version
  • 191 Downloads
  • 2.62 MB File Size
  • 1 File Count
  • July 14, 2016 Create Date
  • July 14, 2016 Last Updated
▼ Scroll for Details ▼

An Improvement of the Velocity Distribution Predicted by Linear Theory for Wings with Straight Subsonic Leading Edges

ARC-CP-418 An Improvement of the Velocity Distribution Predicted by Linear Theory for Wings with Straight Subsonic Leading Edges

FileAction
ARC-CP-418 An Improvement of the Velocity Distribution Predicted by Linear Theory for Wings with Straight Subsonic Leading Edges.pdfDownload 
17,005 Documents in our Technical Library
2729350 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 ...