| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 7050386 | Applied Thermal Engineering | 2013 | 14 Pages |
Abstract
⺠Aero-heating Characteristics are studied based on numerical and experiment methods. ⺠The effects of attack angle and sideslip angle are studied in the present paper. ⺠The influence of attack angle on the aero-heating of nose region can be neglected. ⺠High heat flux is limited in a small region around the stagnation point. ⺠Zero degree sideslip angle is suggested in this paper.
Related Topics
Physical Sciences and Engineering
Chemical Engineering
Fluid Flow and Transfer Processes
Authors
Jian-xia Liu, Zhong-xi Hou, Xiao-qing Chen, Jun-tao Zhang,