Severity: Warning
Message: file_get_contents(https://...@gmail.com&api_key=61f08fa0b96a73de8c900d749fcb997acc09&a=1): Failed to open stream: HTTP request failed! HTTP/1.1 429 Too Many Requests
Filename: helpers/my_audit_helper.php
Line Number: 197
Backtrace:
File: /var/www/html/application/helpers/my_audit_helper.php
Line: 197
Function: file_get_contents
File: /var/www/html/application/helpers/my_audit_helper.php
Line: 271
Function: simplexml_load_file_from_url
File: /var/www/html/application/helpers/my_audit_helper.php
Line: 3165
Function: getPubMedXML
File: /var/www/html/application/controllers/Detail.php
Line: 597
Function: pubMedSearch_Global
File: /var/www/html/application/controllers/Detail.php
Line: 511
Function: pubMedGetRelatedKeyword
File: /var/www/html/index.php
Line: 317
Function: require_once
98%
921
2 minutes
20
The rheological properties of the propellant slurry and droplet dynamics during the casting process play a critical role in the manufacturing of propellants. This study systematically investigated the rheological characteristics of a hydroxyl-terminated polybutadiene (HTPB)-based composite solid propellant slurry and optimized the vacuum casting process through integrated experimental and numerical simulation approaches. Rheological tests revealed shear-thinning behavior, with the Herschel-Bulkley model parameters confirming non-Newtonian fluid characteristics. The addition of coarse ammonium perchlorate (AP) particles caused the slurry viscosity to peak at 41 Pa·s, stabilizing at 17 Pa·s after mechanical mixing. A real-time monitoring system combining machine vision and Kalman filtering demonstrated that increasing the vacuum pressure from 10 to 14 psi enhanced the casting efficiency but reduced the dynamic range of droplet impact forces. Numerical simulations validated experimental data, with a casting time deviation of 6.16%-11.07%. The study confirmed that vacuum pressure regulation optimizes process parameters by balancing casting efficiency and impact forces, providing critical theoretical support for propellant defect control and casting process optimization.
Download full-text PDF |
Source |
---|---|
http://www.ncbi.nlm.nih.gov/pmc/articles/PMC12268399 | PMC |
http://dx.doi.org/10.1021/acsomega.5c03072 | DOI Listing |