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Journals   A B C D E F G H I J K L M N O P Q R S T U V W X Y Z
Journal of Aerospace Power
1000-8055
2001 Issue 3
A Review of Vortex Model Development for Rectangular Turbine Cascades
zhou xun ; han wan jin
..............page:199-204,198
Research and Development of Pulse Detonation Engines
yan chuan jun ; he li ming ; fan zuo ; lei heng ren ; huang xi qiao ; zhang qun
..............page:212-217
Application and Development of Platform Friction Damper for depressing Resonant Vibration of Blades
dan ying chun ; hao yan ping ; zhu zuo gen ; zuo zuo tang
..............page:218-223
Calculation of Turbulent Flow over Three-Dimensional Turbine Rotor Blade Rows with Film Cooling on Unstructured Grids
wang bao guo ; li rong xian ; ma zhi ming ; luo xiao yong
..............page:224-231
Determination of Similarity Criteria for Flow and Heat Transfer of Rotor-Stator Disks System
cai yi ; xu guo qiang ; ding shui ting ; tao zhi
..............page:238-241
Unsteady Numerical Simulation on the Effects of Hot Streak Phenomena on Turbine Stage
dong su yan ; liu song ling ; zhu hui ren
..............page:242-248
Endwall Heat Transfer and Film Cooling Measurements in a Turbine Cascade with InjectionUpstream of Leading Edge
liu gao wen ; liu song ling ; zhu hui ren ;lapworth b l;forest a e
..............page:249-255
Investigation on Compressor Blade Load Distribution in Endwall Regions
zhou zheng gui ; wu guo zuo ; ma ruo long
..............page:256-261
A Non-Linear k-ε-kp Two-Phase Turbulence Model
gu hong xia ; zhou li xing
..............page:267-272
A Study on the Two-Dimensional Thrust Vectoring Nozzle with Secondary Flow Injection
qiao wei yang ; cai yuan hu
..............page:273-278
An Inverse Aeroacoustic Problem on Rotor/Stator Interaction
luo jun ; li xiao dong
..............page:279-282
Effects of Non-Smooth Blades on the Cascade Exit Streamwise Vortex Systems
wen jie ; zhao gui lin ; he long de ; peng hui
..............page:283-286
Numerical Method for Calculating the Burst Speed of Axial-Flow-Type Discs
gu ai jun ; zhang xue ren ; wang ping ; liu si yong
..............page:287-290
A Design Method for Aeroengine Robust Multivariable Digit Controller
wang zuo ; meng qing ming
..............page:295-299,304
Study on Non-Augmented Supersonic Cruise of the 4th Generation Engines
tu qiu ye ; tang di yi
..............page:300-304