naca-report-287

naca-report-287
  • Version
  • 53 Downloads
  • 710.49 KB File Size
  • 1 File Count
  • August 25, 2016 Create Date
  • August 25, 2016 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Report - Theories of Flow Similtude

naca-report-287 Theories of Flow Similtude-1

The laws of comparison of dynamically similar fluid motions are derived by three different
methods based on the same principle and yielding the same or equivalent formulas, In this
report prepared for publication by the National Advisory Committee for Aeronautics, in
June, 1927, are outlined the three current methods of comparing dynamically similar motions,
more especially of fluids, initiated respectively by Newton, Stokes (or Helmholtz), and Rayleigh.
These three methods, viz., the integral, the differential, and the dimensional, are enough alike
to be studied profitably together. They will presently be treated in succession then compared.

FileAction
naca-report-287 Theories of Flow Similtude.pdfDownload 

Comment On This Post

Your email address will not be published.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

naca-report-287

naca-report-287
  • Version
  • 53 Downloads
  • 710.49 KB File Size
  • 1 File Count
  • August 25, 2016 Create Date
  • August 25, 2016 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Report - Theories of Flow Similtude

naca-report-287 Theories of Flow Similtude-1

The laws of comparison of dynamically similar fluid motions are derived by three different
methods based on the same principle and yielding the same or equivalent formulas, In this
report prepared for publication by the National Advisory Committee for Aeronautics, in
June, 1927, are outlined the three current methods of comparing dynamically similar motions,
more especially of fluids, initiated respectively by Newton, Stokes (or Helmholtz), and Rayleigh.
These three methods, viz., the integral, the differential, and the dimensional, are enough alike
to be studied profitably together. They will presently be treated in succession then compared.

FileAction
naca-report-287 Theories of Flow Similtude.pdfDownload 
17,005 Documents in our Technical Library
2848336 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 ...