Journal of Aerospace Power 2003 Issue 4 Linear Regression Analysis Method for Censored Data

Linear Regression Analysis Method for Censored Data
huang wei ; fu hui min

..............page:465-469

Analysis Method for Correlation Coefficient Stationary Series with Unequally Spaced Data
ma xiao bing ; fu hui min

..............page:470-476

Anechoic Chamber in the Inlet Room of Transonic Compressor Rig in Beijing University of Aeronautics and Astronautics
wang tong qing ; bao guo liang ; shi wei

..............page:574-576

Investigation of Resonance Characteristics of Conical Resonance Tube
tong xiao yan ; liang guo zhu ; zhang guo zhou

..............page:570-573

Dynamic Response Study of Flexible Nozzle in a Solid Rocket Motor
shi hong bin ; guan zheng xi ; hou xiao

..............page:563-569

Numerical Method for Coolant Mixing in Turbine Cascade Flow Field
wang song tao ; yan pei gang ; sun zuo zuo ; han wan jin ; wang zhong qi

..............page:558-562

Matching Test of an Aircraft Inlet and Engine on the Ground
jiang yong ; tao zeng yuan ; zhang fa qi ; sang zeng chan ; kong wei dong ; zhang bai ling

..............page:554-557

Method for Quantification of Aeroengine Performance Tendency Monitoring
wang ying jun ; xie shou sheng

..............page:549-553

An Averaged Numerical Difference Method for Detection of Stall Inception
zhang pu ; zhu xue ping ; li ying hong

..............page:546-548

A Mass Addition Approach to the Bypass Turbomachine Through Flow Inverse Design Problem
dan peng ; liu xi yang

..............page:542-545

Multivariable Fuzzy-PID Control for Aeroengine
dong jin ; huang jin quan

..............page:538-541

Study of Adjusting Aeroengine Starting Fuel Supply in the Plateau Area
qiao hong xin ; xia ai guo ; yang li

..............page:534-537

Simulation of Dynamic Performance of a Turbofan Engine
qu yu an ; xie shou sheng ; song zhi ping

..............page:530-533

The Integrated Flight/Propulsion H∞ Controller Design for a New Fighter
guo ying qing ; tian tong jun

..............page:524-529

Design Investigation and Application of an Aeroengine Gas Temperature Control System
jiang cai hong

..............page:519-523

The Interior Heat Transfer Characteristics of Gas Turbine Blade Due to Dense Film Cooling Holes
zhang jing yu ; chang hai ping

..............page:515-518

Experimental Study of a ZS195 Direct-Injection Diesel Engine Fueled with Dimethyl-Ether(DME)
liu xiang yun

..............page:512-514

Discharge Coefficient Measurements of Film Cooling Holes on Blade Surface in a Turbine Cascade
xiang an ding ; zhu hui ren ; liu song ling ; xu du chun ; guo wen

..............page:507-511

The Interior Heat Transfer Characteristics of Gas Turbine Blade Due to Sparse Film Cooling Holes
zhang jing yu ; chang hai ping

..............page:502-506

Experimental Investigation of Flow and Heat Transfer About the Thermal Driving of R12 in Rotating Small-Size Circular Enclosures
mao jun zuo ; chang hai ping ; fang li

..............page:498-501

A Preliminary Study of Nox Emission of staging/Premixed and Prevaporized Lean Combustion Low Emission Combustor Scheme
lin yu zhen ; peng yun zuo ; liu gao en

..............page:492-497

Variable-Dimension Construction in the Axial Arrangement of Finger Seal Mechanism
chen guo ding ; su hua ; zhang yong hong

..............page:488-491

Experimental Study of Low Leakage and High Endurance Brush Seals
guo lin ; kang ning

..............page:485-487

The Study of Layout Method for 3D Engine Accessories
luo qiang ; chen zhi ying

..............page:481-484

Influence of Deviation and Randomness of Crystallographic Orientations on the Strength and Life of Nickel-Base Single Crystal Superalloy Turbine Blades
yue zhu feng ; lv zhen zhou ; yang zhi guo ; cheng xiao ming ; yin ze yong

..............page:477-480