| タイトル | Development of a spinning wave heat engine |
| 本文（外部サイト） | http://hdl.handle.net/2060/19820023452 |
| 著者（英） | Hubbartt, J. E.; Zinn, B. T.; Powell, E. A. |
| 著者所属（英） | Georgia Inst. of Tech. |
| 発行日 | 1982-08-01 |
| 言語 | eng |
| 内容記述 | A theoretical analysis and an experimental investigation were conducted to assess the feasibility of developing a spinning wave heat engine. Such as engine would utilize a large amplitude traveling acoustic wave rotating around a cylindrica chamber, and it should not suffer from the inefficiency, noise, and intermittent thrust which characterizes pulse jet engines. The objective of this investigation was to determine whether an artificially driven large amplitude spinning transverse wave could induce a steady flow of air through the combustion chamber under cold flow conditions. In the theoretical analysis the Maslen and Moore perturbation technique was extended to study flat cylinders (pancake geometry) with completely open side walls and a central opening. In the parallel experimental study, a test moel was used to determine resonant frequencies and radial pressure distributions, as well as oscillatory and steady flow velocities at the inner and outer peripheries. The experimental frequency was nearly the same as the theoretical acoustic value for a model of the same outer diameter but without a central hole. Although the theoretical analysis did not predict a steady velocity component, simulaneous measurements of hotwire and microphone responses have shown that the spinning wave pumps a mean flow radially outward through the cavity. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 82N31328
NAS 1.26:165611
NASA-CR-165611 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/165059 |
