宇航學(xué)院3月29日學(xué)術(shù)報告預(yù)告
發(fā)布日期：2012-03-26
題 目：航空結(jié)構(gòu)設(shè)計的新方法
時 間：2012年3月29日（星期四）上午9:00-11:00
地 點：宇航學(xué)院會議室（3# 教學(xué)樓一層）
報告人：俄羅斯工程院院士，薩馬拉國立航空航天大學(xué)飛行器系結(jié)構(gòu)優(yōu)化教研室主任，卡馬洛夫（Komarov）教授
歡迎各位老師和同學(xué)參加！
Brief Introduction of the Reporter
Professional: The choice of optimal load-carrying scheme of airframe structure. The weight estimation and weight check of airframe structure on early stage of design. FEM-modeling, design of composite airframe structures.
Participated in design and optimization of airframe structure of different type aircraft, including Tupolev 144/154; Beriev – 30/103/200; Ilushin – 76/86/96 etc.
Author of more then 200 science works, Main scientific works:
* OPTIMAL DESIGN. Theory and Application to Materials and Structures. Edited by Valery V. Vasiliev and Zafer Gurdal. Technomic Publishing Co., Inc 851 New Holland Avenue, Box 3535, Lancaster, Pennsylvania 17604 USA, 1999. (Chapter 4. "Design of Aircraft Structures on the Basis of Discrete Model" by Valeri A. Komarov, p.107-155).
* MECHANICAL ENGINEERING. Encyclopedia. Vol. IV-21. Book 2. DESIGN, STRUCTURES and EQUIPMENT of AIRCRAFT and HELICOPTER. Chapter 2.6. Wings. Moscow, Mechanical Engineering, 2004, p. 226-252.
* The Weight Analysis of Aircraft Structures: Theoretical Base. – "POLIOT", 2000, #1, pp. 31-39. (in Russian).
* New Approach to Improving the Aircraft Structural Design Process. AIAA, Journal of Aircraft, March – April 2002, Volume 39, Number 2, pp. 227-233.
* AIRCRAFT DESIGN USING VARIABLE DENSITY MODELS. Aircraft Engineering and Space Technology, to be published in 2012, number 1.
時 間：2012年3月29日（星期四）上午9:00-11:00
地 點：宇航學(xué)院會議室（3# 教學(xué)樓一層）
報告人：俄羅斯工程院院士，薩馬拉國立航空航天大學(xué)飛行器系結(jié)構(gòu)優(yōu)化教研室主任，卡馬洛夫（Komarov）教授
歡迎各位老師和同學(xué)參加！
Brief Introduction of the Reporter
Professional: The choice of optimal load-carrying scheme of airframe structure. The weight estimation and weight check of airframe structure on early stage of design. FEM-modeling, design of composite airframe structures.
Participated in design and optimization of airframe structure of different type aircraft, including Tupolev 144/154; Beriev – 30/103/200; Ilushin – 76/86/96 etc.
Author of more then 200 science works, Main scientific works:
* OPTIMAL DESIGN. Theory and Application to Materials and Structures. Edited by Valery V. Vasiliev and Zafer Gurdal. Technomic Publishing Co., Inc 851 New Holland Avenue, Box 3535, Lancaster, Pennsylvania 17604 USA, 1999. (Chapter 4. "Design of Aircraft Structures on the Basis of Discrete Model" by Valeri A. Komarov, p.107-155).
* MECHANICAL ENGINEERING. Encyclopedia. Vol. IV-21. Book 2. DESIGN, STRUCTURES and EQUIPMENT of AIRCRAFT and HELICOPTER. Chapter 2.6. Wings. Moscow, Mechanical Engineering, 2004, p. 226-252.
* The Weight Analysis of Aircraft Structures: Theoretical Base. – "POLIOT", 2000, #1, pp. 31-39. (in Russian).
* New Approach to Improving the Aircraft Structural Design Process. AIAA, Journal of Aircraft, March – April 2002, Volume 39, Number 2, pp. 227-233.
* AIRCRAFT DESIGN USING VARIABLE DENSITY MODELS. Aircraft Engineering and Space Technology, to be published in 2012, number 1.