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Aero-propulsive modeling for propeller aircraft using flight data
This paper describes methods to identify an integrated propulsion–airframe aerodynamic
model and a decoupled propulsion model for fixed-wing aircraft with propellers using flight …
model and a decoupled propulsion model for fixed-wing aircraft with propellers using flight …
Analysis, optimization, and testing of a tilt-body aircraft
R Zhao, Z Jiao, J **e, K Li, L Zhao, H Zhang, Z Li… - Aerospace Science and …, 2024 - Elsevier
This paper proposes a new multidisciplinary design optimization framework for tilt-bodies to
obtain the optimal combination of geometry and powertrain, achieving both long endurance …
obtain the optimal combination of geometry and powertrain, achieving both long endurance …
High-accurate robust total variation denoising algorithm with adjustable exponential upper bound function for micro-thrust measurement
Z Liu, X Chen, J Xu, C Zhang, L Xu… - IEEE Transactions …, 2023 - ieeexplore.ieee.org
Micro-Newton thrusters are widely utilized in the field of astronautics. Typically, micro-
Newton thrust signal processing aims at the restoration of piecewise constant signals …
Newton thrust signal processing aims at the restoration of piecewise constant signals …
Verifying the effect of wingtip propellers on drag through in-flight measurements
This work presents the effect of wingtip-mounted propellers on the aircraft drag polar,
identified from in-flight measurements. In previous wind-tunnel experiments, significant …
identified from in-flight measurements. In previous wind-tunnel experiments, significant …
SE-ResNet-based noise reduction for steady-state micro-thrust measurement
Z Liu, C Zhang, X Chen, J Xu, L Zhao… - … Conference on Sensing …, 2022 - ieeexplore.ieee.org
Micro-Newton thrusters are widely utilized in the field of astronautics. Typically, the precision
of micro-newton thrust measurement is fundamentally hinged upon the level of background …
of micro-newton thrust measurement is fundamentally hinged upon the level of background …
Advances in Aero-Propulsive Modeling for Fixed-Wing and eVTOL Aircraft Using Experimental Data
BM Simmons - 2023 - vtechworks.lib.vt.edu
Small unmanned aircraft and electric vertical takeoff and landing (eVTOL) aircraft have
recently emerged as vehicles able to perform new missions and stimulate future air …
recently emerged as vehicles able to perform new missions and stimulate future air …
[HTML][HTML] Deep residual shrinkage network with multichannel VMD inputs for noise reduction of micro-thrust measurement
Z Liu, X Chen, J Xu, L Zhao - AIP Advances, 2024 - pubs.aip.org
Micro-newton thrusters are widely utilized in the field of astronautics. Typically, the precision
of micro-newton thrust measurement fundamentally depends on the background noise level …
of micro-newton thrust measurement fundamentally depends on the background noise level …
Experimental evaluation of the drag curves of small fixed wing UAVs
A Weishaeupl, L McLay, A Sobester - The Aeronautical Journal, 2024 - cambridge.org
Tight budgets often limit the scope of test campaigns within the development programmes of
small uncrewed air vehicles (UAVs). This paper explores a range of combinations of …
small uncrewed air vehicles (UAVs). This paper explores a range of combinations of …
Simultaneous Wind Field Measurements with Doppler Lidar, Quadrotor and Fixed-Wing UAV
View Video Presentation: https://doi. org/10.2514/6.2023-0625. vid This study compares the
wind velocity field measurements obtained from a ground-based Doppler Lidar, a fixed-wing …
wind velocity field measurements obtained from a ground-based Doppler Lidar, a fixed-wing …
Design and testing of an in-flight thrust measurement system for a pylon-mounted miniature jet engine
J Bartasevicius, PA Fleig, A Metzner… - AIAA SCITECH 2022 …, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-1827. vid Optimization of aircraft's
performance often requires careful consideration of aerodynamic drag. However, direct …
performance often requires careful consideration of aerodynamic drag. However, direct …