| 发明名称 |
METHOD OF REDUCTION OF THICKNESS OF GAS BOUNDARY LAYER ON STREAMLINED SURFACE |
| 摘要 |
FIELD: experimental aerodynamics. SUBSTANCE: streamlined surface (model under test and/or aerodynamic nozzle) is cooled down to temperatures at which boundary layer of gas is changed into condensed state. EFFECT: more effective results. 1 dwgo
|
| 申请公布号 |
RU2103667(C1) |
申请公布日期 |
1998.01.27 |
| 申请号 |
RU19940032778 |
申请日期 |
1994.09.08 |
| 申请人 |
TSENTRAL'NYJ AEHROGIDRODINAMICHESKIJ INSTITUT IM.P;ROF N E ZHUKOVSKOGO |
发明人 |
KEKHVAJANTS V.G.;KEKHVAJANTS V.G. |
| 分类号 |
G01M9/02;(IPC1-7):G01M9/02 |
主分类号 |
G01M9/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
|
| 地址 |
|
