A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft

Research output: Contribution to journal › Research article › Contributed › peer-review

Contributors

Details

Original languageEnglish
Article number897213
JournalInternational Journal of Aerospace Engineering
Volume2015
Issue number10
Publication statusPublished - 2015
Peer-reviewedYes

External IDs

Scopus 84944214775
ORCID /0000-0003-1185-0046/work/155816257

Keywords