Accession Number:

ADA170157

Title:

Acta Aeronautica et Astronautica Sinica (Selected Articles),

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Report Date:

1986-07-11

Pagination or Media Count:

112.0

Abstract:

Partial contents Wind Tunnel Experimental Investigation on Spanwise Blowing Characteristics of Three-dimensional Turbulent Boundary Layers at Low and Subsonic Speeds Measured by a Straight Wing Erected on a Flat Plate Study of a Multi-color Flow Field Survey Technique Observations on Wake of a Circular Disk during Starting by Hydrogen Bubble Method Measurement of Turbulent Separated Flows with a Two-dimensional LDV System An Experimental Investigation of the Location of the Boundary Layer Transition Area on the Airfoil NACA0012 Using Surface Hot Film Gauges.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE