期刊簡介預(yù)計審稿時間： 12周，或約稿

The Main aim and scope of this Journal is to help improve each separate components R&D and superimpose separated results to get integrated systems by striving to reach the overall advanced design and benefits by integrating: (a) Physics, Aero, and Stealth Thermodynamics in simulations by flying unmanned or manned prototypes supported by integrated Computer Simulations based on: (b) Component R&D of: (i) Turbo and Jet-Engines, (ii) Airframe, (iii) Helmet-Aiming-Systems and Ammunition based on: (c) Anticipated New Programs Missions based on (d) IMPROVED RELIABILITY, DURABILITY, ECONOMICS, TACTICS, STRATEGIES and EDUCATION in both the civil and military domains of Turbo and Jet Engines.

The　International Journal of Turbo & Jet Engines　is devoted to cutting edge research in theory and design of propagation of jet aircraft. It serves as an international publication organ for new ideas, insights and results from industry and academic research on thermodynamics, combustion, behavior of related materials at high temperatures, turbine and engine design, thrust vectoring and flight control as well as energy and environmental issues.

本期刊的主要目的和范圍是幫助改進每個獨立組件的研發(fā)，并將分離的結(jié)果疊加以獲得集成系統(tǒng)，力求通過集成以下方面實現(xiàn)整體先進設(shè)計和效益：（a）通過飛行無人或載人原型進行模擬，在基于以下方面的綜合計算機模擬的基礎(chǔ)上，實現(xiàn)物理學、航空和隱身熱力學：（b）基于以下方面的組件研發(fā)：（i）渦輪和噴氣發(fā)動機、（ii）機身、（iii）頭盔瞄準系統(tǒng)和彈藥：（c）基于以下方面的預(yù)期新計劃任務(wù)：（d）在渦輪和噴氣發(fā)動機的民用和軍用領(lǐng)域提高可靠性、耐用性、經(jīng)濟性、戰(zhàn)術(shù)、戰(zhàn)略和教育。

《渦輪與噴氣發(fā)動機國際期刊》致力于噴氣式飛機傳播理論和設(shè)計的前沿研究。它作為一個國際出版機構(gòu)，發(fā)表有關(guān)熱力學、燃燒、高溫下相關(guān)材料的行為、渦輪機和發(fā)動機設(shè)計、推力矢量和飛行控制以及能源和環(huán)境問題等工業(yè)和學術(shù)研究的新思想、新見解和新成果。

《International Journal Of Turbo & Jet-engines》(國際渦輪與噴氣發(fā)動機雜志)編輯部通訊方式為FREUND PUBLISHING HOUSE LTD, PO BOX 35010, TEL AVIV, ISRAEL, 61350。如果您需要協(xié)助投稿或潤稿服務(wù)，您可以咨詢我們的客服老師。我們專注于期刊咨詢服務(wù)十年，熟悉發(fā)表政策，可為您提供一對一投稿指導(dǎo)，避免您在投稿時頻繁碰壁，節(jié)省您的寶貴時間，有效提升發(fā)表機率，確保SCI檢索（檢索不了全額退款）。我們視信譽為生命，多方面確保文章安全保密，在任何情況下都不會泄露您的個人信息或稿件內(nèi)容。