EXPERIMENTAL INVESTIGATION OF THE FORMATION OF A GAS JET BEHIND THE FRONT OF A SHOCK WAVE IN THE OUTFLOW OF DIVERGENT AND SUPERSONIC NOZZLES,
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Pagination or Media Count:
A shock tube was used in carrying out the investigations. Dimensions of the nozzles used in the experiment are given together with empirical formulas obtained.
- Fluid Mechanics