Посмотр Факультет літакобудування (№ 1) по названию
Отображаемые элементы 29-48 из 1211
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Heavy transport aircraft
(2023)The purpose of the work: the aim of this diploma project is to design a heavy transport aircraft with payload of 100000 kg, including determining the take-off mass and geometric parameters in the zero and first approximations, ... -
Improvement of the repair method of the aircraft components made of polymer composite materials with operational damage
(ХАІ, 2022)The subject of study in this article is the repair method of the aircraft (A/C) components made of polymer com-posite materials (PCM) with operational damage. This article improves the repair method of the A/C PCM components ... -
Investigation of the adaptive wing passenger aircraft and creation of its conception
(2023)The purpose of the work: develop Technical Requirements Specification, to do statistical data analysis of scientists, who dealt with adaptive wing passenger aircraft and what issues they claim, issues, which remained ... -
Investigation of the autorotation stability of a turbofan engine with a detached fan blade
(ХАІ, 2023)One of the requirements for the aircraft being designed is the ability to continue flying and landing if one engine fails. One of the calculated cases of engine failure is the separation of the fan blade. This phenomenon ... -
Light one engine aircraft wing airflow analysis
(2023)In this article, the group briefly introduced the requirements and development of the four-seater aircraft, and completed the design content required by the task through statistical analysis and calculation. Aiming at this ... -
Long-range passenger airplane. Winglet airflow analysis
(2023)The purpose of the work: the aim of the diploma project is to create a long-range passenger aircraft for 450 passengers, including the general views of the projected airplane, the determination of the takeoff mass and ... -
Mass efficiency determination for shear joint
(ХАИ, 2011)Formulae permitting to determine parameters of jointed members and fasteners influence to joint mass are given. -
Mathematical model of a vertical-axial wind motor in a viscous gas flow
(ХАІ, 2022)The development of vertical axial wind turbines in Ukraine is in its infancy for many reasons: the lack of systematic theoretical and experimental studies of the aerodynamic characteristics of various schemes of wind ... -
Mathematical simulation of fuel burn schedule effect on airplane center-of-gravity position
(ХАИ, 2016)Formulas to describe shape of fuel tanks arranged in wings, wing center section and fuselage are proposed on the base of wing shape analysis of real transport category airplanes. Methods of fuel burn sequence designation and ... -
Medium-range passenger aircraft and in-air noise reduction study
(2023)The purpose of the work: The aim of this diploma project is to design a medium-range passenger aircraft with 120 passengers, including determining the take-off mass and geometric parameters in the three approximations, ... -
Numerical simulation of laminated plastics pulse riveting process
(ХАИ, 2007)The list of existent problems within the limits of considered process is brought; the aim and tasks to perform is described; the analysis and analytical model type, the geometrical, physics-mechanical, finite element and ... -
Numerical study of the aerodynamic characteristics of airfoil with high-lift devices
(ХАІ, 2023)The subject matter of this article is the aerodynamic profile of the wing with high-lift devices in the aircraft transport category. -
Pressure feed with gas generator upper stage engine for a hypersonic suborbital cube-sat launch vehicle and sounding rocket «Shivastra-1»
(ХАИ, 2010)An increasing trend, Low cost space access with Microsatellites, and so the need of an efficient, simple, reliable equally cost effective Carrier was considered with rapid designing and fast prototyping design concept so ... -
Selection of optimal center-of-gravity of transport category airplane from minimum required thrust condition
(ХАИ, 2017)Expression for optimum center-of-gravity of transport category airplane at cruise flight mode is created from the condition of minimum required thrust (aerodynamic drag). For example, graph for optimum center-of-gravity ... -
Selection of the rational geometry of specimen for compression test
(ХАІ, 2022)The object of study in this article is the conditions during the compression test. The subject matter is the models that simulate the physical processes during the compression test. The goal is to obtain models, which allow ... -
Solid modeling
(ХАІ, 2008)Тhе general information for study of the basic of the solid modeling of the part and of assemblies for different solid modeling systems is given. The main particularities of the solid modeling applications for such fietds ... -
Study of design features of an electric light aircraft
(2023)The purpose of the work: develop Technical Requirements Specification, research the all electrical assignment, analysis of scientists, who dealt with electrical aircraft and what issues they claim and what problem still ... -
Supersonic business jet general design and aerodynamic characteristics CFD study
(2023)The purpose of the work is to analyze the design features and reliability of the supersonic business jet, also called SSBJ, design its general view, load carrying structure, calculate the aerodynamic and flight characteristics ... -
Sweptback wing stress state
(KhAI, 2013)Guidance manual illustrates how statically indeterminate systems are calculated by the example of a sweptback wing with a root triangle. The authors assume that students already have appropriate knowledge of further ...