Performance Model Identification of the General Electric CF34-8C5B1 Turbofan Using Neural Networks
This paper presents a methodology developed at the Laboratory of Applied Research in
Active Controls, Avionics, and Aeroservoelasticity to identify a performance model of the …
Active Controls, Avionics, and Aeroservoelasticity to identify a performance model of the …
Engine thrust model determination and analysis using a large operational flight database
C Deiler - CEAS Aeronautical Journal, 2023 - Springer
Different engine thrust models are developed from operational flight data with limited a priori
knowledge as part of a novel process for aircraft flight performance model determination …
knowledge as part of a novel process for aircraft flight performance model determination …
New aerodynamic studies of an adaptive winglet application on the Regional Jet CRJ700
This study aims to evaluates how an adaptive winglet during flight can improve aircraft
aerodynamic characteristics of the CRJ700. The aircraft geometry was slightly modified to …
aerodynamic characteristics of the CRJ700. The aircraft geometry was slightly modified to …
Aircraft engine performance model identification using artificial neural networks
View Video Presentation: https://doi. org/10.2514/6.2021-3247. vid This paper presents a
methodology developed at the Laboratory of Applied Research in Active Controls, Avionics …
methodology developed at the Laboratory of Applied Research in Active Controls, Avionics …
A methodology to determine the precision uncertainty in gas turbine engine cycle models
MJG Arrieta, RM Botez - The Aeronautical Journal, 2024 - cambridge.org
This paper proposes a methodology to define and quantify the precision uncertainties in
aerothermodynamic cycle model comparisons. The total uncertainty depends on biases and …
aerothermodynamic cycle model comparisons. The total uncertainty depends on biases and …
Method for calculating aircraft flight trajectories in presence of winds
This paper presents a practical method to compute the four-dimensional flight trajectories of
aircraft in the presence of winds. The proposed method consisted of numerically integrating …
aircraft in the presence of winds. The proposed method consisted of numerically integrating …
Improved local scale generic cycle model for aerothermodynamic simulations of gas turbine engines for propulsion
MJ Gurrola Arrieta, RM Botez - Designs, 2022 - mdpi.com
A local scale Aerothermodynamic Generic Cycle Model (AGCM) is proposed. The AGCM
accounts for several improvements not considered in similar models, such as compressor …
accounts for several improvements not considered in similar models, such as compressor …
New generic turbofan model for high-fidelity off-design studies
M Gurrola-Arrieta, RM Botez - AIAA AVIATION 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-3642. vid In this paper, a high-
fidelity aerothermodynamic Off-Design Generic Model is proposed. The model was …
fidelity aerothermodynamic Off-Design Generic Model is proposed. The model was …
Cessna Citation X takeoff and departure trajectories prediction in presence of winds
This paper presents a method developed at the Laboratory of Applied Research in Actives
Controls, Avionics, and AeroServoElasticity for calculating takeoff and departure trajectories …
Controls, Avionics, and AeroServoElasticity for calculating takeoff and departure trajectories …
In-house high-fidelity generic turbofan model for aerothermodynamic design studies
M Gurrola-Arrieta, RM Botez - AIAA SciTech 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-0774. vid In this paper, the
methodology and results of a new generic model for aerothermodynamic design point …
methodology and results of a new generic model for aerothermodynamic design point …