Calculation of the gasdynamic and thermal characteristics of a resonance tube with supersonic jet impingement
Abstract
A theoretical study is presented on the influence of thermal effects, due to supersonic jet impingement, on the gasdynamic characteristics of a resonance tube. Theoretical values for amplitude and period of oscillations are compared with experimental data.
- Publication:
-
Leningradskii Universitet Vestnik Matematika Mekhanika Astronomiia
- Pub Date:
- January 1981
- Bibcode:
- 1981VeLen.......59V
- Keywords:
-
- Aerothermodynamics;
- Jet Impingement;
- Resonance;
- Supersonic Jet Flow;
- Tubes;
- Amplitudes;
- Gas Heating;
- Gas Temperature;
- Mach Number;
- Fluid Mechanics and Heat Transfer