Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Fanil Ishmuratov"'
Publikováno v:
TsAGI Science Journal. 50:181-193
Autor:
Frederico Afonso, Alessandro Airoldi, Salvatore Ameduri, Gianluca Amendola, Gennady A. Amiryants, Francesco Amoroso, Alexandre Antunes, Alfonso Apicella, Gianvito Apuleo, Maurizio Arena, Uwe T.P. Arnold, Silvestro Barbarino, Marco Bellucci, Paolo Bettini, Robert Blackwell, Ruxandra M. Botez, Miguel Á. Castillo Acero, Vasily Chedrik, Alexander Chedrik, Alexander Chevagin, Monica Ciminello, Antonio Concilio, Alessandro De Gaspari, Federico Martín de la Escalera, Luca Angelo Di Landro, Ignazio Dimino, José Lobo do Vale, Antoine Dumont, Roman Efimov, Sergio Esposito, Yasser Essa, Rolf Evenblij, Alessandro Gilardelli, André Gratias, Teodor L. Grigorie, Generoso Iannuzzo, Fanil Ishmuratov, Vladimir Kulesh, Innokentiy Kursakov, Ksenia Kuruliuk, Svetlana Kuzmina, Fernando Lau, Thomas H. Lawrence, Leonardo Lecce, Grace Lima, Peter F. Lorber, Andreas Lühring, Alexander Lysenkov, Marco Magnifico, Vladimir Malenko, Victor Malyutin, Mihir P. Mistry, Christof Nagel, Maria Chiara Noviello, Felipe Odaguil, Antonio Pagano, Damiano Pasini, Modesto Pecora, Rosario Pecora, Fabian Peter, Mikhail Pronin, Francesco Rea, Sergio Ricci, Lorenzo Rossi, Salvatore Russo, Giuseppe Sala, Andrey Saprykin, Oliver Schorsch, Martin Schueller, Sergey Shalaev, Stefan Storm, Tobias Strobl, Eike Stumpf, Afzal Suleman, Viktor Timokhin, Maurizio Verrastro, Andrea Vigliotti, William A. Welsh, Matthew L. Wilbur, Mikhail Zichenkov
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6add9ae250cd75a4b5cef7d672002236
https://doi.org/10.1016/b978-0-08-100964-2.09991-3
https://doi.org/10.1016/b978-0-08-100964-2.09991-3
Autor:
Ksenia Kuruliuk, Andrey Saprykin, Innokentiy Kursakov, Roman Efimov, Alexander Lysenkov, Victor Malyutin, Svetlana I. Kuzmina, Alexander Chevagin, Viktor Pavlovich Timokhin, Vladimir Kulesh, Vasily V. Chedrik, Vladimir Malenko, Alexander Chedrik, Mikhail Zichenkov, Gennady A. Amiryants, Mikhail Pronin, Fanil Ishmuratov, Sergey Shalaev
Wind tunnel testing of adaptive wing/aircraft structures has been carried out at TSAGI with the aim of investigating, demonstrating and assessing novel concepts, enabling cost-effective aerodynamic designs through the use of adaptive/morphing wings,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::877589d40d4930da0dd86efe9f9c95f0
https://doi.org/10.1016/b978-0-08-100964-2.00023-x
https://doi.org/10.1016/b978-0-08-100964-2.00023-x
Publikováno v:
12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference.
In the framework of multidisciplinary design environment the mathematical models of civil airplanes with high aspect ratio wings have been developed. They have been used for design optimization with taking into consideration lift-to-drag, loads, stre
Publikováno v:
11th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference.
*† ‡ An overview of multidisciplinary approach to design of different types of wings of passenger airplanes and application of this approach in the preliminary design phase are presented. Applications illustrate some aspects of the using multidis
Publikováno v:
47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 14th AIAA/ASME/AHS Adaptive Structures Conference 7th.
*† ‡ § This paper describes dynamic effectiveness of wing tip controls as the capability to influence on accelerations and loads. The favorable effects of aeroelasticity were demonstrated on analytical and experimental studies of dynamically-sim
Publikováno v:
10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference.
Publikováno v:
10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference.
The main purpose of this work is to develop an effectiv e procedure for computation and optimization of induced drag of an elastic airplane, as well as to consider different methods to realize drag optimum values. On the base of the standard panel me
Publikováno v:
Scopus-Elsevier
This paper concentrates on researches of aeroelasticity characteristics of heavy passenger aircraft with taking into account aerodynamic nonlinearities. The mathematical models of the baseline airplane and of its dynamically scaled model intended for
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3469fe97f6a5711ccb7b02473c6228c2
http://www.scopus.com/inward/record.url?eid=2-s2.0-34547497834&partnerID=MN8TOARS
http://www.scopus.com/inward/record.url?eid=2-s2.0-34547497834&partnerID=MN8TOARS