TY - JOUR
T1 - Base aerodynamic behavior and its effects on performance of aerospike nozzle
AU - Wang, Chang Hui
AU - Liu, Yu
AU - Liao, Yun Fei
PY - 2004/10
Y1 - 2004/10
N2 - Base pressure of a two-cell tile-shaped aerospike nozzle was measured under conditions of 10°, 20°,30°,40° cell inclination and 0.0%,0.4%,1.0%,1.4%,2.0%,3.0% base bleed ratio. It was found that in the base region there exists open wake, close wake or open to close transition condition under different ambient pressure. Base aerodynamic behavior does not change with the variation of cell inclination or base bleed ratio. Experimental performance change with altitude of two-cell linear aerospike nozzle truncated at 80%,40%,30% and 20% of the full plug length was obtained. The performance of the experimental aerospike nozzle and the pressure distribution along the plug were also computed. The predicted performance shows good agreement with measured data. Based on experiments and numerical simulation, the effects of plug truncation and base aerodynamic behavior on the performance of the aerospike nozzle are investigated.
AB - Base pressure of a two-cell tile-shaped aerospike nozzle was measured under conditions of 10°, 20°,30°,40° cell inclination and 0.0%,0.4%,1.0%,1.4%,2.0%,3.0% base bleed ratio. It was found that in the base region there exists open wake, close wake or open to close transition condition under different ambient pressure. Base aerodynamic behavior does not change with the variation of cell inclination or base bleed ratio. Experimental performance change with altitude of two-cell linear aerospike nozzle truncated at 80%,40%,30% and 20% of the full plug length was obtained. The performance of the experimental aerospike nozzle and the pressure distribution along the plug were also computed. The predicted performance shows good agreement with measured data. Based on experiments and numerical simulation, the effects of plug truncation and base aerodynamic behavior on the performance of the aerospike nozzle are investigated.
KW - Aerospace propulsion system
KW - Aerospike nozzle
KW - Base aerodynamic behavior
KW - Experiment
KW - Performance change with altitude
KW - Rocket engine
UR - https://www.scopus.com/pages/publications/10444290647
M3 - 文章
AN - SCOPUS:10444290647
SN - 1000-8055
VL - 19
SP - 724
EP - 729
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 5
ER -