To analyze three-dimensional internal flow characteristic of spherical convergent flap nozzles with hexagonal and bowtie geometries
the geometric models were established and N-S equation and S-A model were employed in the numerical simulation.The simulation was developed at different NPR(nozzle pressure ratio).The calculated results are compared favorably well with experimental data.Furthermore
the internal flow characteristic and performance of two nozzles are compared and analyzed.
Numerical simulation of internal flow field in gas generator of fire extinguishing bomb
Computation of effect of different nozzle parameters on internal performance of convergent-divergent axisymmetric nozzle
Numerical simulation on effects of variable specific heat capacity on internal flow field of jet vector nozzle
Effects of gap between nozzles on plug heat transfer characteristics
Analysis of overall aerodynamic performance of axial-flow compressor with attenuated blade tip
Related Author
Yunfeng LI
Kangqing DENG
Ruihua LU
Peiwen QIN
Chunliang GUO
Lifan YAN
Changlong HUANG
SHAO Wan-ren
Related Institution
Key Laboratory of Aerospace Chemical Power Technology, Hubei Institute of Aerospace Chemical Techologh, China Aerospace Science and Technology Corporation,Xiangyang Hubei
Hubei Institute of Aerospace Chemistry Technology, China Aerospace Science and Technology Corporation,Xiangyang Hubei
Shenyang Aeroengine Research Institute, Aviation Industry Corporation of China
Missile Institute, Air Force Engineering University, Sanyuan Shanxi
School of Astronautics, Beijing University of Aeronautics and Astronautics