INITIAL EXPENDABLE TURBOJET PROTOTYPE TESTING EXPIRIENCES
Proceedings of 41st Danubia-Adria Symposium Advances in Experimental Mechanics (pp. 83-86) АУТОР(И) / AUTHOR(S): Nikola Davidović , Nenad Kolarević , Milos Stanković , Marko Miloš Download Full Pdf DOI: 10.46793 УВОД / INTRODUCTION: Expendable turbojets, typically in thrust range from…
