Доступ предоставлен для: Guest
TsAGI Science Journal

Выходит 6 номеров в год

ISSN Печать: 1948-2590

ISSN Онлайн: 1948-2604

COMPARATIVE WEIGHT ANALYSIS OF FUSELAGE SECTIONS WITH DIFFERENT STRUCTURE LAYOUTS

Том 50, Выпуск 3, 2019, pp. 309-323
DOI: 10.1615/TsAGISciJ.2019031092
Get accessGet access

Краткое описание

The results of forming a methodology and calculation algorithm to estimate the weight efficiency of fuselage sections with an advanced structure layout based on comparative analysis with alternative structure layouts are presented. Application of the developed methodology to estimate the weight efficiency of a lattice composite fuselage section of a passenger aircraft is shown.

ЛИТЕРАТУРА
  1. Final Report Summary, ALASCA (Advanced Lattice Structures for Composite Airframes), Grant agreement ID: 265881, https://cordis.europa.eu/project/rcn/97744/reporting/en.

  2. Final Report Summary, POLARBEAR (Production and Analysis Evolution for Lattice Related Barrel Elements under Operations with Advanced Robustness), Grant agreement ID: 605448, https://cordis.europa.eu/project/rcn/111110/reporting/en.

  3. Fomin, V., Shanygin, A., and Zamula, G., Multilevel Approach for Strength and Weight Analyses of Composite Airframe Structures, in Proc. of 27th International Congress of the Aeronautical Sciences, Nice, France, Sept. 19-24, 2010.

  4. Fomin, V., Multi-Modeling Approach in Pre-Designing of Fuselage Wing Section Consisted of Stiffened Composite Panels, in Proc. of 3rd Aircraft Structural Design Conference of Royal Aeronautical Society, Delft, Netherlands, 2012.

  5. Dubovikov, E., Novel Approach and Algorithm for Searching Rational Nonconventional Airframe Concepts of New Generation Aircrafts, in Proc. of 28th International Congress of the Aeronautical Sciences, Brisbane, Australia, 2012.

  6. Dubovikov, E., Fomin, V., Kondakov, I., Shanygin, A., and Zichenkov, M., Shell of Sealed Fuselage Compartment from Composites, Russian Patent RU 2558493, Federal Service for Intellectual Property, Russian Federation, 2015.

  7. Chernov, A., Dubovikov, E., Fomin, V., Kondakov, I., and Shanygin, A., System of Protection of Airframe Load-Bearing Composite Elements, Russian Patent RU 2558494, Federal Service for Intellectual Property, Russian Federation, 2015.

  8. Dubovikov, E., Fomin, V., Kondakov, I., and Shanygin, A., Weight Analysis of Alternative Fuselage Barrels on the Basis of the Multilevel Algorithm, in Proc. of the 3rd EASN Association International Workshop on Aerostructures, Milan, Italy, October 9-11, 2013.

  9. Fomin, V., Ierusalimsky, K., Karpova, G., and Zamula, G., Analyzing the Effect of Skin Post-Buckling on General Stresses, Strains and Stability of Composite Structures, NASA Technical Report NCC1-233 ID 20010000336, 1998.

  10. Fomin, V.P., Computing Cylindrical Stiffened Skins Accounting for Non-Linear Behavior of Structural Elements, Uch. Zap. TsAGI, 11(1):72-80, 1980.

  11. Zamula, G.N. and Iyerusalimskii, K.M., To Stability Computation of Ribbed Cylindrical Skins, Uch. Zap. TsAGI, 12(3):83-94, 1981.

  12. Dubovikov, E. and Fomin, V., Strength Analysis Technique for High Loaded Elements of Composite Airframes, in Proc. of 29th Congress of the International Council of Aeronautical Sciences (ICAS-2014), Saint Petersburg, Russia, 2014 (CD-ROM).

  13. Kondakov, I.O., Development and Validation of Numerical Method for Strength Analysis of Lattice Composite Fuselage Structure, Nauch. Vestn. MGTU GA, 19(6):137-146, 2016.

  14. Dubovikov, E., Fomin, V., and Kondakov, I., FE Modeling of Lattice Composite Fuselage Elements for General and Local Strength Analyses, in Proc. of 3rd EASN Association International Workshop on AeroStructures, Milano, Italy, 2013.

Последний выпуск

KIRILL IVANOVICH SYPALO−50TH ANNIVERSARY NUMERICAL STUDY OF THE DISTURBANCES GENERATED BY MICROJETS IN A SUPERSONIC FLAT-PLATE BOUNDARY LAYER Andrei Valerievich Novikov, Alexander Vitalyevich Fedorov, Ivan Vladimirovich Egorov, Anton Olegovich Obraz, Nikolay Nikolaevich Semenov ANALYSIS OF THE MOVING DETONATION INTERACTION WITH TURBULENT BOUNDARY LAYERS IN A DUCT ON THE BASIS OF NUMERICAL SIMULATION Vladimir Anatolievich Sabelnikov, Vladimir Viktorovich Vlasenko, Sergey Sergeyevich Molev EXPERIMENTAL STUDY OF COUNTERFLOW BLOWING IN HIGH-SPEED FLOW THROUGH AN ASYMMETRIC SLOT IN THE LEADING EDGE OF A SHARP WEDGE Eduard Borisovich Vasilevskii, Ivan Valeryevich Ezhov, Pavel Vladimirovich Chuvakhov ASYMPTOTIC SOLUTIONS TO HYPERSONIC BOUNDARY LAYER EQUATIONS ON A FLAT WING WITH A POINT OF INFLECTION ON THE LEADING EDGE Georgiy Nikolaevich Dudin, Aleksey Vyacheslavovich Ledovskiy WAVE MODEL OF ORGANIZED STRUCTURES IN A TURBULENT BOUNDARY LAYER ON A PLATE WITH ZERO LONGITUDINAL PRESSURE GRADIENT Vladimir Alekseevich Zharov, Igor Ivanovich Lipatov, Rami Salah Saber Selim NUMERICAL SIMULATION OF THE FLOW AROUND LANDSCAPE FRAGMENTS AND SOLUTION VERIFICATION Viktor Viktorovich Vyshinsky, Koang T'in' Zoan POLYNOMIAL REPRESENTATION OF THERMODYNAMIC PROPERTIES OF COMBINED FUEL SYSTEMS IN RAMJET SIMULATION MODELS Timur Romanovich Zuev, Mikhail Semenovich Tararyshkin A MODEL TEST METHODOLOGY FOR THE INVESTIGATION OF AN ELASTICALLY SCALED MAIN ROTOR Maxim Andreyevich Ledyankin , Sergey Anatolyevich Mikhailov, Dmitry Valeryevich Nedel'ko, Timur Arturovich Agliullin INDEX, VOLUME 51, 2020
Портал Begell Электронная Бибилиотека e-Книги Журналы Справочники и Сборники статей Коллекции Цены и условия подписки Begell House Контакты Language English 中文 Русский Português German French Spain