AEDC-TR-77-96

  • Version
  • 51 Downloads
  • 2.93 MB File Size
  • 1 File Count
  • July 18, 2017 Create Date
  • July 18, 2017 Last Updated
Scroll for Details

Arnold Engineering Development Center, Technical Report - The Calculation of Compressible Transitional, Turbulent, and Relaminarizational Boundary Layers Over Smooth and Rough Surfaces using an Extended Mixing Length Hypothesis

FileAction
AEDC-TR-77-96 The Calculation of Compressible Transitional, Turbulent, and Relaminarizational Boundary Layers Over Smooth and Rough Surfaces using an Extended Mixing Length Hypothesis.pdfDownload 

Comment On This Post

Your email address will not be published.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

AEDC-TR-77-96

  • Version
  • 51 Downloads
  • 2.93 MB File Size
  • 1 File Count
  • July 18, 2017 Create Date
  • July 18, 2017 Last Updated
Scroll for Details

Arnold Engineering Development Center, Technical Report - The Calculation of Compressible Transitional, Turbulent, and Relaminarizational Boundary Layers Over Smooth and Rough Surfaces using an Extended Mixing Length Hypothesis

FileAction
AEDC-TR-77-96 The Calculation of Compressible Transitional, Turbulent, and Relaminarizational Boundary Layers Over Smooth and Rough Surfaces using an Extended Mixing Length Hypothesis.pdfDownload 
17,005 Documents in our Technical Library
2757938 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 ...