This paper describes criteria and formulas that are capable of evaluating the burning perimeters of cruciform and Inform solid propellant grains (externally burning grains) during combustion. The effect of the restrictor width on the burning perimeter during combustion is investigated and analyzed. Some dimensions of the grain configuration are optimized and recommended.
A-N., Z. (2001). GEOMETRIC ANALYSIS OF CRUCIFORM AND TRIFORM SOLID PROPELLANT GRAINS. International Conference on Aerospace Sciences and Aviation Technology, 9(ASAT Conference, 8-10 May 2001), 1-13. doi: 10.21608/asat.2001.24778
MLA
ZAYED A-N.. "GEOMETRIC ANALYSIS OF CRUCIFORM AND TRIFORM SOLID PROPELLANT GRAINS", International Conference on Aerospace Sciences and Aviation Technology, 9, ASAT Conference, 8-10 May 2001, 2001, 1-13. doi: 10.21608/asat.2001.24778
HARVARD
A-N., Z. (2001). 'GEOMETRIC ANALYSIS OF CRUCIFORM AND TRIFORM SOLID PROPELLANT GRAINS', International Conference on Aerospace Sciences and Aviation Technology, 9(ASAT Conference, 8-10 May 2001), pp. 1-13. doi: 10.21608/asat.2001.24778
VANCOUVER
A-N., Z. GEOMETRIC ANALYSIS OF CRUCIFORM AND TRIFORM SOLID PROPELLANT GRAINS. International Conference on Aerospace Sciences and Aviation Technology, 2001; 9(ASAT Conference, 8-10 May 2001): 1-13. doi: 10.21608/asat.2001.24778
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