Acta Aerodynamica Sinica,
Abstract
Partial contents: Separation criteria for 3-D steady viscous flow and flow behavior near separation line; Aerodynamic calculation of airfoil with separation; Numerical simulation of vortex breakdown; Environmental study on turbulent boundary layer separation; Turbulent boundary layer characteristics in and out of separation region measured at wing-plate junction at low and subsonic speeds; Effect of winglet on spatial vortex of a solid in rotation at high angle of attack; Investigation of separated flow in the base; Advances in inverse boundary layer techniques; Wing leading edge vortex breakdown; Numerical analysis of a 3-D separated flow; Exact vortex solutions of the Navier-stokes solutions; Characteristic analysis of separated flow; A method computing viscous interaction with laminar separation; Numerical computation of exended Kalman Filter and its application to aerodynamic parameter identification of a reentry satellite; Relaxation phenomenon behind a bow shock wave in dusty gas; A simple formula of drag coefficient of sphere in rarefied hypersonic flow; Alleviation and control of asymmetric load at high angle of attack. Keywords: Aerodynamics, Chinese translations; Chinese periodicals.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 03, 1986
- Accession Number
- ADA174599
Entities
People
- Chen Bingyong
- Shi Xungang
- Zhang Bingxuan
- Zhang Hanxin
- Zhu Ziqiang
Organizations
- National Air and Space Intelligence Center