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Tyre heat of multi-wheel bogie undercarriage at touchdown
Almost all studies on tyre heat during aircraft touchdown are based on the assumption that the tyres touch the ground simultaneously, and the...
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Efficient multidisciplinary modeling of aircraft undercarriage landing gear using data-driven Naïve Bayes and finite element analysis
Advancements in aircraft design and production necessitate exhaustive simulations of critical components, such as landing gear, to ensure optimal...
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Thermal Penetration of Aircraft Tyre Tread at Touchdown
Most studies of friction and heat conduction in aircraft tyres at touchdown are limited to the tread surface. However, it is necessary to know the...
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Introduction to Aircraft Loads
The basic understanding of the significance of aircraft loads and their relationship to aeroelasticity will be elaborated comprehensively. The...
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Aspects of yaw control design of an aircraft with distributed electric propulsion
Distributed electric propulsion (DEP) offers new options in aircraft design. Besides the optimization of the wing, another area of optimization is...
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Aerodynamics and Aircraft Control
This chapter covers basic aerodynamics, aircraft stability, dynamic response, longitudinal and lateral control and response, powered flying controls,...
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Laser Beam as a Precision Tool to Increase Fatigue Resistance in an Eyelet of Undercarriage Drag Strut
The article contains the results of tests on a laser-processed eyelet of undercarriage drag strut to increase its fatigue strength. Laser processing...
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Configurational Aspects and Vehicle Specific Investigations for Future Unmanned Cargo Aircraft
This chapter focuses on the work done to examine in more detail how three configurations, namely double tail boom fixed wing aircraft, box wing...
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Bird Impact Analysis of a Typical Transport Aircraft Wing
Bird striking event is one of the most dangerous risks to the safety of aircrafts. Although most of the bird strike events involve relied small birds...
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Symplectic Methods for a Finite-Dimensional System
In this chapter, symplectic approaches for the finite-dimensional Hamiltonian systems are discussed. Firstly, the foundations of the symplectic...
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Flight Test Data Comparison
The aim of this Chapter is to investigate whether the results from, and the observations about, the Fuji FA – 200 -160 are generalizable to the other...
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Evaluating Stabilizing Effects of Geosynthetics in Flexible Airport Pavement Structures by FE Analyses
Geosynthetic reinforcements have demonstrated their effectiveness in enhancing road pavement structures through mechanical stabilization. However,...
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Gust alleviation by spanwise load control applied on a forward and backward swept wing
The present paper investigates the feasibility of gust load alleviation at transonic speeds on a backward swept and a forward swept transport...
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Adverse effect of rainfall on aerodynamic characteristics for different NACA airfoil configurations—A comprehensive review
The frenzied demand for the transit of humans and commodities in this modern world requires aircraft to operate in adverse weather conditions of...
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Innovation and Application of Vehicle Panoramic Intelligent Detection System in Air Defense Inspection for Airport Rapid Transit System
Currently, there is no rapid transit vehicle scanning device used for airport air defense inspections both domestically and internationally. The air...
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Unmanned Air Vehicles
Unmanned air vehicles (UAVs) have become increasingly important in both civil and military roles. UAVs depend totally on avionic systems in order to...
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Locating method and motion stroke design of flexible assembly tooling for multiple aircraft components
To get an accurate dimensional size/shape/spatial and assembly accuracy, flexible assembly tooling is developed and applied in aviation production,...
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The Method of Triads in the Aircraft Design
The article describes the features of the triad method application at the initial stages of aircraft design for the selection of fundamental...
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State Estimation Using Filtering Methods Applied for Aircraft Landing Maneuver
State estimation methods are the popular means of validating aerodynamic characteristics on maneuvering Aircraft. This work deals with adaptation of...
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Validation of the safety requirements of the landing gear using fault tree analysis
We analyze the functionality of the landing system of a regional aircraft in the extension and cruise flight modes and validate safety requirements...
