Acta Aeronautica et Astronautica Sinica (Selected Articles),
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 11, 1986
- Accession Number
- ADA170157
Entities
People
- Deng Xueying
- Li. Xiangrui
- Tian Xueshi
- Xin Dingding
- Zhao Jincheng
Organizations
- National Air and Space Intelligence Center