| タイトル | Thermal and fluid flow analyses of sounding rocket experiment 74-21/2R and 74-21/3R |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790016124 |
| 著者（英） | Robertson, S. J. |
| 著者所属（英） | Lockheed Missiles and Space Co. |
| 発行日 | 1979-04-01 |
| 言語 | eng |
| 内容記述 | The thermal convective velocities during the 4-21/2R and 74-21/3R flight tests were calculated. The 74-21/2R and 74-21/3R ground tests were analyzed using a convection formula. Thermal convection velocities of 0.1 to 0.5 cm/sec were calculated for the 74-21/2R and 74-21/3R ground tests which were two to four orders of magnitude greater than for the flight tests. For the 74-21/2R flight test, solutal effects do not produce any convective motion. For the 74-21/3R flight test closed form convection equations estimated the solutal convective velocities on the order of 1/0.003 cm/sec. |
| NASA分類 | FLUID MECHANICS AND HEAT TRANSFER |
| レポートNO | 79N24295
NASA-CR-161224
LMSC-HREC-TR-D568959 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/175522 |
