[PDF][PDF] Cessna citation X climb and cruise performance improvement using adaptive winglet
This research is conducted with the global idea of improving Cessna Citation X
performances required to perform a typical climb or cruise phase. As part of this project, the …
performances required to perform a typical climb or cruise phase. As part of this project, the …
[HTML][HTML] Low-fidelity design optimization and development of a VTOL swarm UAV with an open-source framework
N Sethi, S Ahlawat - Array, 2022 - Elsevier
Hybrid configurations in aircraft design are highly favorable as they can achieve the
appropriate trade-offs required to develop a generalized unmanned aerial system (UAS) …
appropriate trade-offs required to develop a generalized unmanned aerial system (UAS) …
Efficient Aerodynamic Analysis for Propeller Aircraft Including Viscous Effects
GL Olichevis Halila, L Neves Pedreiro… - AIAA SCITECH 2022 …, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-0429. vid The aerodynamic design
of subsonic, propeller-driven aircraft must account for relevant effects such as the interaction …
of subsonic, propeller-driven aircraft must account for relevant effects such as the interaction …
[PDF][PDF] Aerodynamic Modeling of an Aircraft using Open Foam: A High Fidelity Open Source Software–Application on the CRJ-700
VIATION has improved over the decades thanks to the use of aircraft modeling techniques
and methodologies [1–5]. Aerodynamics is one aspect of aircraft design that must be very …
and methodologies [1–5]. Aerodynamics is one aspect of aircraft design that must be very …
[PDF][PDF] Conceptual Design Synthesis of Electric VTOL Aircraft for Urban Air Mobility
O Ugwueze - 2022 - pureportal.coventry.ac.uk
The emerging field of electric vertical take-off and landing (eVTOL) aircraft design lacks the
wealth of data that traditional fixed-wing aircraft and rotorcraft design methodologies draw …
wealth of data that traditional fixed-wing aircraft and rotorcraft design methodologies draw …
Méthodes originales pour déterminer la forme d'un profil d'aile
En vue d'appliquer la technologie d'aile déformable sur l'empennage horizontal du Cessna
Citation X, le LARCASE devait mettre au point un modèle aérodynamique précis de …
Citation X, le LARCASE devait mettre au point un modèle aérodynamique précis de …
Original Methods for Finding a Wing Shape Airfoil
In view of the future application of a morphing wing technology on the horizontal tail of the
Cessna Citation X, the LARCASE team had to develop an accurate aerodynamic model of …
Cessna Citation X, the LARCASE team had to develop an accurate aerodynamic model of …