Development and Validation of an Open Source CFD Code for Analysis of Aerospace Vehicles

CHM Souza, AC Romano, A Passaro… - Journal of Aerospace …, 2023 - SciELO Brasil
In this work, a review of the theoretical aspects and an assessment to validate a
Computational Fluid Dynamics (CFD) open-source code for applications in aerospace …

[HTML][HTML] Data-Driven Sparse Sensor Placement Optimization on Wings for Flight-By-Feel: Bioinspired Approach and Application

AC Hollenbeck, AJ Beachy, RV Grandhi… - Biomimetics, 2024 - mdpi.com
Flight-by-feel (FBF) is an approach to flight control that uses dispersed sensors on the wings
of aircraft to detect flight state. While biological FBF systems, such as the wings of insects …

[HTML][HTML] Performance improvement of turbo energy recovery device in desalination using flow field simulation and uniform design experiment

S Wang, Y **ao, C Wang, Y Li, Q Ma, X Luo - Desalination and Water …, 2025 - Elsevier
As the core equipment of seawater desalination, the turbine energy recovery device (TERD)
exerts a crucial impact on the energy consumption of desalination system. The study aims to …

Vortex dynamics study and flow visualization on aircraft model with different canard configurations

SB Wibowo, B Basuki, Sutrisno, TA Rohmat… - Fluids, 2021 - mdpi.com
Canard configuration on fighter planes is essential for regulating flow and the occurrence of
vortex interactions on the main wing, one of which is to delay stall. Stall delays are useful …

Wind Tunnel Aerodynamic Study of a VTOL-UAV for Wide Range of Angles of Attack and Sideslip Angles: (EMERGENTIa project)

VM Prieto, S Esteban - Aerotecnica Missili & Spazio, 2021 - Springer
This article presents the design, manufacturing and wind tunnel tests conducted on a 1: 4
scaled Vertical Take Off and Landing (VTOL) Unmanned Aerial Vehicle (UAV). A brief …

[PDF][PDF] Sutrisno

SB Wibowo, B Basuki - Rohmat, TA - academia.edu
Canard configuration on fighter planes is essential for regulating flow and the occurrence of
vortex interactions on the main wing, one of which is to delay stall. Stall delays are useful …

[PDF][PDF] EFFECT OF LENGTH AND DIAMETER OF AIRCRAFT FUSELAGE ON DRAG AND LIFT COEFFICIENT BY CFD

G Brinda, APA Amalan - researchgate.net
Present work aimed to analysis the aerodynamic drag and lift coefficient of large turbo
propeller aircraft fuselage through Computational Fluid Dynamics (CFD) analysis (ANSYS …