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Abstrakty
To solve the problem of AC aerodynamically shaped envelope design the integrated system of design was developed that allows minimizing human involvement in routine operations of modeling and calculation of design parameters.
Słowa kluczowe
Czasopismo
Rocznik
Tom
Strony
61--65
Opis fizyczny
Bibliogr. 6 poz., il., wykr.
Twórcy
autor
- Lviv Polytechnic National University
autor
- Lviv Polytechnic National University
autor
- Lviv Polytechnic National University
Bibliografia
- 1. D.P. Raymar, 2002, Aircraft design - a conceptual approach, American Institute of Aeronautics and Astronautics, Washington D.C. 2002.
- 2. Brusov V. S. Baranov S. K. 1989, Optimalnoye proyektirovaniye letatelnykh apparatov: Mnogotselevoy podkhod // Moskva, Mashinostroyeniye, 1989.
- 3. Piyavskiy S.A., Brusov V.S, Khvilon Ye.A., 1974, Optimizatsiya parametrov mnogotselevykh letatelnykh apparatov. M.: Mashinostroyeniye, 1974.
- 4. Melnyk M., 2013, Analysis of the Relevance of Developing Tools for Computer-Aided Design of Airships / M. Melnyk, A. Stefanskyi, A. Kernytskyy // Perspective Technologies and Methods in MEMS Design (MEMSTECH), 2013 Proceedings of IXth International Conference, 16–20 April. 2013, Polyana-Svalyava, - pp. 151-152.
- 5. M. Melnyk, A. Stefanskyi, A. Kernytskyy; 2013, Study of transverse edges of rigidity (frames) for aok case and of their rational selection construction // Proceeding of the VII-th International Symposium on Mechanics of Materials and Structures, June 3-6, 2013, Augustow, Poland,- pp. 140-141.
- 6. Husynin V.P., 2010, Systemy povitryanoho startu raket-nosiyiv lehkoho klasu // Naukovi visti NTUU “KPI”. - 2010. - 1. s. 140-146.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-36bd41b4-45b2-4272-926d-57851c5fc58c