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[HTML][HTML] On the selection of aircraft-engine pairs for medium-haul Low-Cost Carriers operations
The selection of aircraft and engine models poses a significant challenge for Low-Cost
Carriers (LCCs) striving for profitability. This decision is compounded by numerous …
Carriers (LCCs) striving for profitability. This decision is compounded by numerous …
Black widow optimization for reducing the target uncertainties in localization wireless sensor networks
Abstract Localization Wireless Sensor Networks (WSN) represent a research topic with
increasing interest due to their numerous applications. However, the viability of these …
increasing interest due to their numerous applications. However, the viability of these …
Aerodynamic Shape Optimization of Subsonic/Supersonic Flows Integrating Variable-Fidelity Longitudinal Trim Analysis
Most existing studies on aerodynamic shape optimization have not considered longitudinal
trim under control surface deflection, typically achieving self-trim through a constraint of zero …
trim under control surface deflection, typically achieving self-trim through a constraint of zero …
Hybrid Fuzzy-Based Method for Optimally Selecting Aircraft for Low-Cost Carriers Operating Medium-Haul Flights
Abstract The proliferation of Low-Cost Carriers (LCCs) is generating a new business
paradigm in the air transport sector by promoting lower airfares. Those LCCs have to …
paradigm in the air transport sector by promoting lower airfares. Those LCCs have to …
[PDF][PDF] Parametric Study of NACA 4-Series Airfoil Designs for Lift-to-Drag Performance
Airfoil design has a great influence on the overall flight performance of flying vehicles. In
conceptual design stage where design decisions have to be quickly made, having a …
conceptual design stage where design decisions have to be quickly made, having a …
Anti-vibration Design of the Civil Aircraft's Horizontal Tail Trailing Edge Compartment
Y Lyu, F Yu, Y Chen - Journal of Physics: Conference Series, 2023 - iopscience.iop.org
The horizontal tail trailing edge compartment is a vital component of civil aircraft, situated
between the horizontal tail beam and elevator. Its primary function is to connect the elevator …
between the horizontal tail beam and elevator. Its primary function is to connect the elevator …
Research on Lift Error of Horizontal Tail Based on Component Disassembly Method
Q Wen, K Yang, Z Cheng, Y Zhang - China Aeronautical Science and …, 2022 - Springer
It is very important for calculating aerodynamic load and strength design to obtain
aerodynamic force of aircraft components accurately. The aerodynamic force of horizontal …
aerodynamic force of aircraft components accurately. The aerodynamic force of horizontal …
Dynamic performance analysis of aircraft chassis based on 3D simulation technology
W Song, J Sun - … on Mechanical Design and Simulation (MDS …, 2023 - spiedigitallibrary.org
As an important part of the aircraft, the analysis of its dynamic performance is also extremely
critical. As the core component of the aircraft, the performance of the aircraft chassis plays a …
critical. As the core component of the aircraft, the performance of the aircraft chassis plays a …