Journal of Propulsion Technology 2011 Issue 4 Erosion and deposition of carbon-carbon nozzle inserts in low-thrust long-duration solid rocket motors

Erosion and deposition of carbon-carbon nozzle inserts in low-thrust long-duration solid rocket motors
zhang xiao guang ; wang chang hui ; liu yu ; xiong wen bo ; ren jun xue

..............page:586-590

Influence of bleed hole location on heat transfer in rectangular channels with ribs
zhang zong wei ; zhu hui ren ; wang zhen wei ; guo tao

..............page:581-585

Methodology of dynamic ablation test for insulation material
sun xiang yu ; zhang zuo ; hu shu fang ; wang de ; chen si ; xiong hong chao

..............page:597-600

A reaction dynamic adaptive chemistry modeling method based on sensitivity analysis
gou xiao long ; shi wan ling ; gui ying

..............page:534-538

Experiment on combustion performance of a ramjet prototype combustor in low pressure condition
niu zhi gang ; fei li qun ; feng shou yi ; he xiao min

..............page:509-511,524

Numerical simulation of clocking effect on turbine wake transportation process
li wei ; zuo xiao cheng ; wang hui bin ; ou yang hua ; du chao hui

..............page:471-478

Analysis of combustion efficiency for ducted rocket
wang yu qing ; li li han ; liu ming zuo ; he yong pan

..............page:520-524

Experiment on atomization characteristics of high density hydrocarbon
feng shou yi ; niu zhi gang ; fei li qun ; liu yong

..............page:512-519

Investigation of infrared suppression of exhaust system by reducing surface temperature and emissivity
huang wei ; ji hong hu ; si ren ; chen jun

..............page:550-556

Numerical study on the swirl flow combustion characteristics of solid fuel ramjet
liu wei ; yang tao

..............page:504-508

Rupture life reliability of HP-turbine for a turbo-fan engine with influence of the stress relaxation
lu shan ; zhao ying chun ; fan zuo

..............page:491-496

Thermal-stress analysis on two-way rotation axis variable throat area flow control valves
tang jin lan ; yu jia ; li jin xian ; feng xi ping

..............page:591-596

Design and simulation of a new novel engine adaptive model
zhang hai bo ; chen zuo zuo ; sun jian guo ; wu wei chao

..............page:557-563

Experiment on liquid sheet breakup process of pressure swirl injector
liu juan ; li qing lian ; liu wei dong ; wang zhen guo

..............page:539-543

Test on aging fracture properties of HTPB propellant
chang xin long ; yu yan feng ; zhang you hong ; long bing

..............page:564-568

Experiment on convective coefficient of different turbine blade trailing edges
sun rui jia ; yang wei hua ; he yi hong ; hao xu sheng ; li wei

..............page:485-490

Computational and experimental analysis of the flow field in shock vector control nozzle
liu hui ; xing yu ming

..............page:544-549

Experiments on ignition performance of ramjet combustor
li chun guang ; ji hong hu ; wang jian ; zhang zhen jia

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

Numerical investigation on difference between blade leading edge vortex and normal impingement cooling
liu gao wen ; xue biao ; peng li ; xia quan zhong

..............page:576-580,585

Integration performance analysis of typical arrangement inlet/missile
jiang ni ; wang yong wei ; ling wen hui ; wang jian

..............page:451-454

Adaptive passive control on hypersonic inlet boundary layer separation
su wei yi ; zhang wang yuan ; jin zhi guang

..............page:455-460

Reduction of kerosene detailed combustion reaction mechanism based on DRG and QSSA
liu jian wen ; xiong sheng wei ; ma xue song

..............page:525-529,549

Insulator material screen experiments and ablation characteristic under high acceleration condition
liu yang ; li jiang ; he guo qiang ; li qiang ; sun xiang yu ; hu shu fang

..............page:569-575

Numerical simulation on effects of oscillatory angle of attack on performance of hypersonic inlet
li ting he ; gao rui ze ; li zuo na

..............page:461-465,496

Experimental investigation for the effects of different unsteady source in centrifugal compressor
zhou li ; zhang zuo ; cai yuan hu

..............page:497-503

Film cooling effectiveness experiment of impingement effusion cooling in curved section
cao jun ; yang wei hua ; shi rui ; hao xu sheng ; song shuang wen

..............page:479-484

tui jin ji shu tou gao zhi nan

..............page:F0003-F0003

Numerical investigation of blade vibration response induced by inlet distortion in axial compressor
zhang ming ming ; hou an ping ; wang qiang

..............page:466-470,503