FUSELAGE SHAPE OPTIMIZATION AIMED AT WING-FUSELAGE CONFIGURATION DRAG REDUCTION AT SUPERSONIC SPEEDS by N. D. Ageev, A. A. Pavlenko

“…The problem of fuselage shape optimization of the wing-body configuration is considered in the following three formulations. …”
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LAYOUT of the PASSENGER twin-fuselage AIRPLANE FOR LOCAL LINES by V. G. Gusev

“…The article shows the peculiarities and disadvantages of the classical single-fuselage configuration aircraft for local lines. It also provides an overview of the twin-fuselage configuration aircraft. …”
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TO THE DEVELOPMENT OF AERODYNAMIC SHAPE OF MEDIUM SIZED PERSPECTIVE HELICOPTER FUSELAGE by V. A. Vershkov, M. S. Makhnev, D. V. Petrukhin

“…The dependencies of the fuselage component drag, such as the bow, fairings exhaust pipes of helicopter, sponsons, and tail sectionof the fuselage, on their form are described in this article.At the second stage the fuselage geometry was created in program SolidWorks. …”
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Determination of durability of samples modeling the MS-21 fuselage longitudinal and cross joints by V. K. Harina

“…To determine the durability of the samples, modeling the MS-21 fuselage longitudinal and cross joints, theoretical calculations and experimental studies were carried out, and it allowed to judge about the compliance of the results obtained by the loaded hole.…”
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DEVELOPMENT AND VALIDATION OF NUMERICAL METHOD FOR STRENGTH ANALYSIS OF LATTICE COMPOSITE FUSELAGE STRUCTURES by I. O. Kondakov

“…Lattice composite fuselage structures are developed as an alternative to conventional composite structures based on laminated skin and stiffeners. …”
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COMPUTING EXPERIMENT FOR ASSESSMENT OF AERODYNAMIC CHARACTERISTICS OF SEPARATE ELEMENTS IN THE STRUCTURE OF THE FUSELAGE OF A HELICOPTER by V. A. Ivchin, V. G. Sudakov, A. A. Ryzhov

“…The present publication describes the calculation of helicopter fuselage aerodynamic characteristics and its separate elements, by computing experiment. …”
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Development of parametric criteria for assessing aircraft damage in a collision with birds by Yu. V. Esipov, E. A. Bochkova, A. Yu. Medvedev

“…When a bird strikes with a mass of at least 1 kg and at a mutual speed equal to or greater than 50 m/s, the destruction of the fuselage will occur with a probability measure of 1.0, and when the pilot is exposed to the fuselage fragments, it may hurt him and the ship may fall. …”
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A FIRST APPROXIMATION CALCULATION OF AIR CUSHION CHASSIS WEIGHT OF TRANSPORT AIRPLANE by V. P. Morozov, Y. Y. Merzlikin

“…The algorithm can be expanded to include additional design decisions, such as the transformation of the fuselage, increasing the air cushion chassis canopy due to extensions, center of gravity, etc.…”
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QUALITY INFLUENCE OF SURFACE ON AIRCRAFT TAKE-OFF by V. G. Tsipenko, N. I. Chekalova

“…The main part of the system is a unit for calculating increments of aerodynamic coefficients caused with changing of technical condition of the surface of the airframe (roughness, waviness, available protruding elements on the airframe surface, etc.) and residual deformation of the wing, fuselage, vertical and horizontal tail, as well as the difference between the rods symmetrically operating engines. …”
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Improving the reliability of a visual inspection of damaged aircraft structural components made of composite materials by I. A. Davydov

“…The new designs of aircraft, which have been put into service thus far, feature 50 % and more composite materials of the airframe mass and use monolithic carbon fiber composite panels for the fuselage skin. Carbon fiber composite is particularly sensitive to the post-impact compressive strength reduction, and the operating aircraft environment is characterized by an array of sources of impact damages. …”
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Electrooptical complex for terrain on-time survey by S. B. Stukalov, D. S. Stukalov, V. I. Kondrikov, R. S. Gavryushin

“…The downward-looking cameras of visible and infrared bands, integrated into the UAV fuselage belly are used for the surface monitoring and survey. …”
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Solution of the optimization problem for the purpose of designing a lattice polymer composite structure with the outer skin by A. A. Skleznev, A. A. Chervyakov, I. G. Agapov

“…Such structures are mass-produced and used as load-bearing bodies of space vehicles or fuselage compartments of atmospheric aircraft of advanced structural design. …”
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NOVEL APPROACH TO DESIGN OF LIGHTWEIGHT AND RELIABLE COMPOSITE PRIMARY AIRCRAFT STRUCTURES by M. Ch. Zichenkov, I. O. Kondakov, A. N. Shanygin

“…The application of the novel approach allowed to obtain a number of lightweight solutions for the structure of cylindrical fuselage section of civil aircraft and for the hermetic cabin of the "Flying wing" aircraft.…”
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Effect of engine failure on aerodynamic characteristics of a light transport aircraft model by Yu. S. Mikhailov

“…The aircraft is equipped with a loading ramp with a relatively short flat rotatable part of the lower fuselage surface. Experimental studies of the longitudinal and lateral characteristics of the model with installed simulators of a power plant were carried out in TsAGI low-speed wind tunnel T-102. …”
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DAMAGE OF THE AIRCRAFT STRUCTURAL SYSTEM BY LIGHTING WITH RAIN PRECIPITATION ON ITS SURFACE by S. K. Kamzolov, S. M. Novikov, A. N. Razumovsky

“…The presence of condensation (moisture, ice) on the surface of the aircraft can significantly increase the damage of fuselage skin resulting from the electromechanical impact of lightning, which was confirmed by the results of the experimental research conducted at the Chair of Physics of the Moscow State Technical University of Civil Aviation. …”
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Shear Angle Effect on the Engineering Constants of Woven Fabrics by Johnson Ezenwankwo, Iva Petrikova, Josef Zak

“…It is therefore, pertinent to investigate the effect of some key parameters on the engineering constants of a material, especially when they are used for HSE critical purposes such as reinforced composites employed in the design of aircraft wings, fuselages and other parts. The effect of shear angle on the six engineering constants is investigated using Ansys Material Modeler. …”
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