NUMERICAL ANALYSIS OF HEATING SHOCK ON NOSE OF AEROSPACE PROJECTILES

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HOMAYOONFAR M.; MIRZAEI M.

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

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Paper Information

Journal: Journal of Aerospace Mechanics Year:2014 | Volume:10 | Issue:2 (36) Page(s): 41-50

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Title

NUMERICAL ANALYSIS OF HEATING SHOCK ON NOSE OF AEROSPACE PROJECTILES

Author(s)

HOMAYOONFAR M. | MIRZAEI M. | Issue Writer Certificate

Keywords

THERMAL STRESSQ2

NOSEQ2

ABLATIONQ1

AERODYNAMIC HEATINGQ2

Abstract

In this article THERMAL STRESS of graphite NOSE of aerospace projectiles is investigated. The governing equations, boundary conditions, rate of surface recession, ABLATION model of graphite, and also moving mesh generation are described. In order to calculate THERMAL STRESS, at first unsteady heat transfer equation in an unstructured moving mesh is solved using finite volume method for reentry period, then the results of the thermal analysis are transferred to a structure analysis software. Aerodynamic pressure is applied as a variable with time and position and THERMAL STRESS is calculated for the reentry flight. There is a good agreement between the current results and those of the other researchers.

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APA: Copy

HOMAYOONFAR, M., & MIRZAEI, M.. (2014). NUMERICAL ANALYSIS OF HEATING SHOCK ON NOSE OF AEROSPACE PROJECTILES. AEROSPACE MECHANICS JOURNAL, 10(2 (36)), 41-50. SID. https://sid.ir/paper/101729/en

Vancouver: Copy

HOMAYOONFAR M., MIRZAEI M.. NUMERICAL ANALYSIS OF HEATING SHOCK ON NOSE OF AEROSPACE PROJECTILES. AEROSPACE MECHANICS JOURNAL[Internet]. 2014;10(2 (36)):41-50. Available from: https://sid.ir/paper/101729/en

IEEE: Copy

M. HOMAYOONFAR, and M. MIRZAEI, “NUMERICAL ANALYSIS OF HEATING SHOCK ON NOSE OF AEROSPACE PROJECTILES,” AEROSPACE MECHANICS JOURNAL, vol. 10, no. 2 (36), pp. 41–50, 2014, [Online]. Available: https://sid.ir/paper/101729/en

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