Coherent structures generated by a circular jet issuing into a cross laminar boundary layer L. E. BrizziJ. L. BousgarbièsE. Foucault OriginalPaper Pages: 81 - 85
Effect of nonequilibrium homogenous condensation on flow fields in a supersonic nozzle Toshiaki SetoguchiShigeru MatsuoHiroyuki Hirahara OriginalPaper Pages: 90 - 96
Shock-boundary layer interaction control, predictions using a viscous-inviscid interaction procedure and a Navier-Stokes solver G. SimandirakisB. BourasK. D. Papailiou OriginalPaper Pages: 97 - 110
Aerodynamic optimum design of transonic turbine cascades using Genetic Algorithms Li JunFeng ZhenpingShen Zuda OriginalPaper Pages: 111 - 116
Uniform Deterministic Discrete Method for three dimensional systems Ben-Wen LiWen-Quan TaoYu-Hong Nie OriginalPaper Pages: 117 - 122
The Second-order Imaginary Plane Method and its calculation accuracy Dong PengChen XiaodongQin Yukun OriginalPaper Pages: 123 - 127
Reexamination of correlations for nucleate site distribution on boiling surface by fractal theory Yang Chunxin OriginalPaper Pages: 128 - 131
Fuel economy opportunities for internal combustion engines by means of oil-cooling C. F. MaJ. C. LiJ. Chen OriginalPaper Pages: 132 - 140
Static and transient performance prediction for CFB boilers using a Bayesian-Gaussian Neural Network Haiwen YeWeidou Ni OriginalPaper Pages: 141 - 148
Numerical study of the effect of imaginary circle diameter and initial flow field on the aerodynamic field in a tangentially fired furnace Zhu TongSun ShaozengMa Xichen OriginalPaper Pages: 149 - 154