Unsteady flow computations on a flying projectile within a ballistic range

DOI10.1016/S0045-7930(97)00055-8zbMath0971.76057OpenAlexW1986964731WikidataQ127797556 ScholiaQ127797556MaRDI QIDQ1974654

Yoko Takakura, Satoru Ogawa, Fumio Higashino

Publication date: 13 November 2000

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0045-7930(97)00055-8

zbMATH Keywords

shock waveunsteady flowsprojectileblast wavemulti-domain techniqueballistic rangeeffect of virtual massflying speedmoving coordinate methodsupersonic launch

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) Gas dynamics (general theory) (76N15) Supersonic flows (76J20)

Cites Work

• Unnamed Item
• An analysis of finite-difference and finite-volume formulations of conservation laws
• Damped Euler-equation method to compute transonic flow around wing-body combinations

This page was built for publication: Unsteady flow computations on a flying projectile within a ballistic range