The Proceedings of the 2021 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2021), Volume 1

This proceeding comprises peer-reviewed papers of the 2021 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2021), held from 15-17 November 2021 in Jeju, South Korea. This book deals with various themes on computational fluid dynamics, wind tunnel testing, flow visualization, UAV...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Körperschaft: SpringerLink (Online service)
Weitere Verfasser: Lee, Sangchul (HerausgeberIn), Han, Cheolheui (HerausgeberIn), Choi, Jeong-Yeol (HerausgeberIn), Kim, Seungkeun (HerausgeberIn), Kim, Jeong Ho (HerausgeberIn)
Format: Elektronisch E-Book
Sprache:Englisch
Veröffentlicht: Singapore : Springer Nature Singapore : Imprint: Springer, 2023.
Ausgabe:1st ed. 2023.
Schriftenreihe:Lecture Notes in Electrical Engineering, 912
Schlagworte:
Online-Zugang:https://doi.org/10.1007/978-981-19-2689-1
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Inhaltsangabe:
  • Asia-Pacific Region’s Aircraft Design and Development Strategy for Single-Aisle Aircraft in the Oligopoly Market of Boeing and Airbus
  • Study on wind resistance characteristics of Multi-rotor UAV
  • Inverse Design Method of Transonic Airfoil Based on Deep Neural Network,- High-rise Building Wind Field Simulation
  • Study on Aerodynamic Characteristics of “Propeller/Wing” System with Overset Meshes Method
  • An Ontology Based Single Source of Truth (SSOT) Construction Approach for Aircraft Modeling and Simulation
  • Experimental Investigations on Aerodynamic and Psychoacoustic Characteristics of Loop-Type Propeller
  • Effect of Dynamic Micro Vortex Generator on Corner Shock Wave Boundary Layer Interactions Based on DES
  • Aerodynamic Characteristics of a Compound Deflected LEF/TEF Rotor
  • Analysis of Aerodynamic Characteristics and Influence of Parameters of the Quad Tiltrotor Aircraft
  • A Two-step Optimization Method Using POD-based GeometricParameterization for Aerodynamic Shape Optimization
  • Anti-Icing Performance of Engine Inlet Cone by Hot Air Film
  • Aerodynamic characteristics of close UAV formation
  • Conceptual design and system level analysis of tilt-duct eVTOL aircraft
  • Research on Wind Tunnel Test of the Total Pressure Probe Layout for Civil Aircraft
  • Study on the Dynamic Aerodynamic Performance of Airfoil with Direct Force Measurement
  • The Research of Correlationship and Critical Ice Shape Acquisition in CIRA-IWT Icing Wind Tunnel.