Journal of Aerospace Power 2002 Issue 2 Aerodynamic Design of High Load Transonic Compressor Stage

Aerodynamic Design of High Load Transonic Compressor Stage
li zuo jiang ; qi dai ; deng bao yang ; jing rong qiang ; gui xing min

..............page:183-187

Numerical Methods for Three-Dimensional Viscous Rotor/Stator Interactions in Turbomachinery
ren yu xin ; wang zhu

..............page:178-182

Study on the Method Establishing the Revolution Difference Map for a Two-Spool-Turbojet Engine
wang hua qing ; chen mao zhang

..............page:173-177

Analysis of Distortion Test Data by Inlet Flat Baffle
wang ru gen ; jiang yong ; zhang qi fa

..............page:170-172

The Analysis of Economic Performance Properties of Engines
li shi wu

..............page:165-169

Study of Selecting Parameters and Fault Diagnosis for Turboshaft
li ben wei ; hu guo cai ; gao guo sheng ; hou zhi qiang ; gao yong

..............page:160-164

Experimental Investigation of Exhaust Jet Infrared Suppression for Supersonic Flow
yang xu ; xia huan ming ; liu de zhang

..............page:155-159

Numerical Simulation and Design for Aerospike Nozzle
zheng meng wei ; zhang yang jun ; zhu ge wei lin ; zhang bao ning ; liu yu ; zhu sen yuan

..............page:150-154

Study and Application of Calculation Method for Adjusting the Matching Parameters of Turbine Nozzle Area and Engine Nozzle Radius
wang hua qing ; chen mao zhang

..............page:145-149

Study on Contact Ratio of Spiral Bevel Gears and Influence of Pitch Error
deng xiao zhong ; fang zong de ; ren dong feng ; wei bing yang

..............page:268-272

Temperature and Velocity Measurements in Arcjets
chen li ming ; zhao wen hua ; dang dao yuan

..............page:263-267

An Optimum Method for Low Flow High Speed Centrifugal Pump
yuan jun zuo ; zhang zhen peng ; zhang chun liang

..............page:259-262

Investigation on Fault Reasoning for Power System Used in Space Vehicles
zhang chun liang ; zhang zhen peng ; yuan jun zuo ; zhu gang

..............page:255-258

Robust H∞/H2 Mixed Control for Aeroengine Parameter Uncertainty Systems
wang zuo ; chen hua rong

..............page:250-254

Heat Transfer and Pressure Drop of Short Pin-Fin Array with Different Diameter and Shape
zhu hui ren ; xu du chun

..............page:246-249

Interaction between Boiling Bubbles on a Heated Wire
wang zuo ; peng xiao feng

..............page:240-245

Impingement Fluid Characteristics from Rib Roughened Surface within Arrays of Circular Jet
zhang jing yu ; chang hai ping ; zhou chang chun

..............page:236-239

Numerical Simulation of High Temperature Phase Change Heat Storage System
xing yu ming ; xu zuo ; yuan xiu gan ; cui hai ting ; zhang yun hao

..............page:231-235

Ground Simulation Testing of Solar Receiver for the Space Station
xing yu ming ; yuan xiu gan ; cui hai ting ; hou xin bin ; wang chang he

..............page:226-230

Traveling-Wave Vibration of Rotating Shells by Finite Element Method
cao hang ; zhu zuo gen

..............page:222-225

Experimental Study on Acceleration Mobility Measurements for Rotor/Fuselage Coupled Model of Helicopter
gu zhong quan ; yuan sheng tao

..............page:217-221

The Experimental Investigation of Using Suction Surface Fences to Control Secondary Flow in Compressor Cascade
zhong jing jun ; wang hui she ; liu hui juan ; li wei jun ; wang zhong qi

..............page:188-191

A Numerical Model for Duct Fan Vortex Intensity
tu qiu ye ; tang di yi

..............page:192-195

The Principal Component Analysis Method for Engine Flight Mission Profiles Categorization
song ying dong ; gao de ping

..............page:196-200

The Joint Acceptance Function in Response Analysis of Cylindrical Shell Excited by Noise
cao mao guo ; li lin

..............page:201-204

Experimental Research of Bending and Torsional Vibrations of a Double Disc Rotor Due to Rotor-to-Stator Contacts
deng xiao wen ; liao ming fu ;robert liebich;robert gasch

..............page:205-211

Aeroengine Composite Maneuver Loading Spectrum Derivation
song ying dong ; gao de ping

..............page:212-216