The Method of Characteristics (MOC) was applied to the aerospike nozzle.Some particular cases of the aerospike nozzle boundary conditions
expansive wave
oblique shock wave
and so on were considered.Typical flow fields of the aerospike nozzle were obtained.A method of thrust calculation was proposed.The results computed were compared with the experimental data.It is shown that the method is reliable and effective.
AN EQUIVALENT MECHANIC MODEL OF DOUBLE EXTENDIBLE NOZZLE
Solving transient second air system in engine by characteristics method
Numerical computation and analysis of three-dimensional wall temperature of impingement+identical flow convection+film composite cooling
Numerical study on the mixing characteristics of chevron mixers for the afterburner
Numerical investigation on film cooling effectiveness at suction surface of stator blade
Related Author
Yan Deyuan
Zhang Yanyu
Zhang Jingsheng
Zhang Xiaohong
WU Hong
HU Xiao-xiao
WANG Mei-juan
SONG Shuang-wen
Related Institution
th Dept.Beijing University of Aeronautics and Astronautics
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
China Aviation Powerplant Research Institute, Aviation Industry Corporation of China
Shenyang Aeroengine Research Institute, Aviation Industry Corporation of China
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics