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NTIS 바로가기IOP conference series. Materials science and engineering, v.887, 2020년, pp.012009 -
Kretov, Anatolii
AbstractThe work is devoted to the rapid assessment of the weight of the aircraft and its design. This problem occurs when creating new aircraft or in the process of constructive improvement of existing ones. To determine the mass of the entire aircraft, the method of “mass change coefficients...
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Raymer 838 2006 4
Gogolin 160 11 1973
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Evaluation of Anisogric Composite Lattices Structures Weight Effectiveness Using the Load-carrying Factor (Proc. Engineering) Boldyrev 185 153 2017
A Parametric Aircraft Fuselage Model for Ppreliminary Sizing and Crashworthiness Applications (CEAS Aeronaut J) Schwinn 7 357 2016
Preliminary Design of Composite Fuselage Structures Using Analytical Rapid Sizing Methods (CEAS Aeronaut J) Quatmann 2 231 2011
Achternbosch 2003
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