Methane-oxygen detonation characteristics at elevated pre-detonation pressures

被引:12
|
作者
Schumaker, S. Alexander [1 ]
Knisely, Andrew M. [2 ]
Hoke, John L. [2 ]
Rein, Keith D. [3 ]
机构
[1] Air Force Res Lab, Bldg 490,1790 Loop Rd N, Wright Patterson AFB, OH 45433 USA
[2] Innovat Sci Solut, Wright Patterson AFB, OH 45433 USA
[3] Spectral Energies, Wright Patterson AFB, OH 45433 USA
关键词
Detonations; Methane-oxygen; Cell size; Detonation speed; Absorption Spectroscopy; IGNITION; PROPAGATION;
D O I
10.1016/j.proci.2020.07.066
中图分类号
O414.1 [热力学];
学科分类号
摘要
The detonation characteristics of methane-oxygen mixtures at pre-detonation pressures of 101-1,013 kPa were investigated in a detonation tube. Both pure methane-oxygen mixtures and mixtures with argon dilution were explored. Measurements made include cell sizes via soot foil, wave speed via high speed ion probes / pressure transducers, and temperature / H2O molar concentration profiles via 100 kHz absorption spectroscopy. Measured cell widths agreed with predicted cell widths based on a ZND length correlation. In addition, the power law fit of cell width with pre-detonation pressure agreed with previous data at less than 101 kPa. Measured detonation wave speeds agreed within 3% of Chapmen-Jouguet for all cases. H2O molar density and temperature were successfully captured up to 507 kPa. However, above 507 kPa pre-detonation pressure, low signal to noise ratio and poor spectral fits at the extreme conditions of the von Neumann spike resulted in unacceptable uncertainty. These results provide a unique dataset to validate kinetics models and high-fidelity computation fluid dynamics codes for methane-oxygen detonations at elevated pre-detonation pressures relevant to rotating detonation rocket engines. Published by Elsevier Inc. on behalf of The Combustion Institute.
引用
收藏
页码:3623 / 3632
页数:10
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