Loading...
Please wait, while we are loading the content...
Similar Documents
Study of mixing enhancement observed with a co-annular nozzle configuration
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Papamoschou, D. Zaman, K. B. M. Q. |
| Copyright Year | 2000 |
| Description | Jet spreading enhancement with a certain coannular nozzle configuration has been explored. When the outer nozzle is flaired (i.e., made convergent-divergent) the ensuing jet spreads faster than the case where the outer nozzle is convergent. The spreading enhancement is most pronounced when the outer flow is run near 'transonic' condition, in an overexpanded state. Under this condition, the increased spreading takes place regardless of the operating conditions of the inner jet. This observation, first made in a small scale facility, has been confirmed and studied in some detail in a larger-scale facility. Results of the latter experiment are presented in this paper. The spreading increase is shown to be substantial and comparable to or better than that achieved by a lobed nozzle. Estimates based on idealized flow indicate that there is an accompanying thrust penalty - the actual penalty is expected to be less than the estimate but remains undetermined at this time. In both the earlier and the present experiments, the spreading increase has often been found to accompany a flow resonance. The nature of this resonance is addressed in this paper. It is shown that the spreading increase takes place even if the resonance is absent. Thus, flow excitation due to the resonance is ruled out as the underlying mechanism. While the complete mechanism remains unclear, it is conjectured that pressure gradients near the nozzle, characteristic of overexpanded flow, are at the root of the phenomenon. |
| File Size | 789872 |
| File Format | |
| Language | English |
| Publisher Date | 2000-01-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Thermodynamics Nozzle Design Mass Flow Rate Nozzle Flow Spreading Annular Nozzles Annular Flow Mach Number Sound Pressure Pressure Gradients Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |