Unsteady aerodynamic modeling at high incidence for flight dynamic analysis

2001 ◽  
Author(s):  
A. Pashilkar
Keyword(s):  
Dynamic Analysis ◽  
Aerodynamic Modeling ◽  
Unsteady Aerodynamic ◽  
High Incidence

Surrogate Unsteady Aerodynamic Modeling with Autoencoders and LSTM Networks

2022 ◽  
Author(s):  
Huseyin E. Tekaslan ◽  
Yusuf Demiroglu ◽  
Melike Nikbay
Keyword(s):  
Aerodynamic Modeling ◽  
Unsteady Aerodynamic

Unsteady aerodynamic modeling and control of the wind turbine with trailing edge flap

2018 ◽  
Vol 10 (6) ◽  
pp. 063304 ◽  
Author(s):  
Wenguang Zhang ◽  
Yifeng Wang ◽  
Ruijie Liu ◽  
Haipeng Liu ◽  
Xu Zhang
Keyword(s):  
Wind Turbine ◽  
Trailing Edge ◽  
Modeling And Control ◽  
Aerodynamic Modeling ◽  
Unsteady Aerodynamic ◽  
Trailing Edge Flap ◽  
And Control

Unsteady aerodynamic modeling and control of pusher and tilt-rotor quadplane configurations

2019 ◽  
Vol 94 ◽  
pp. 105421 ◽  
Author(s):  
Yunus Govdeli ◽  
Sheikh Moheed Bin Muzaffar ◽  
Raunak Raj ◽  
Basman Elhadidi ◽  
Erdal Kayacan
Keyword(s):  
Modeling And Control ◽  
Tilt Rotor ◽  
Aerodynamic Modeling ◽  
Unsteady Aerodynamic ◽  
And Control

Continuous-time state-space unsteady aerodynamic modeling based on boundary element method

2012 ◽  
Vol 36 (5) ◽  
pp. 789-798 ◽  
Author(s):  
Meysam Mohammadi-Amin ◽  
Behzad Ghadiri ◽  
Mostafa M. Abdalla ◽  
Hassan Haddadpour ◽  
Roeland De Breuker
Keyword(s):  
Boundary Element Method ◽  
State Space ◽  
Boundary Element ◽  
Continuous Time ◽  
Aerodynamic Modeling ◽  
Unsteady Aerodynamic ◽  
Element Method

Dynamics and vibrations of structures with bonded piezoelectric strips subjected to mechanical and unsteady aerodynamic loads

2010 ◽  
Vol 225 (3) ◽  
pp. 625-638 ◽  
Author(s):  
D Mateescu ◽  
Y Han ◽  
A Misra
Keyword(s):  
Dynamic Analysis ◽  
Crack Detection ◽  
Piezoelectric Actuators ◽  
Element Formulation ◽  
Aerodynamic Loads ◽  
Unsteady Aerodynamic ◽  
Wing Structures ◽  
Piezoelectric Strip ◽  
Wing Structure ◽  
The Time Domain

This article presents an analysis of the dynamics of damaged structures with bonded piezoelectric strips executing flexural oscillations generated by mechanical loads, piezoelectric actuators or unsteady aerodynamic loads. These oscillations can be used to detect the presence of cracks for structural health monitoring. The proposed method of crack detection uses pairs of piezoelectric strip sensors bonded on the opposite sides of the structure and is based on the fact that the presence of a crack causes a difference between the strains measured by the two sensors of a pair. The structural analysis presented in this article uses a non-linear model for the cracks and a finite-element formulation for the piezoelectric strips coupled with the structure. A panel method is used to determine the unsteady aerodynamic loads acting on the oscillating wing structure. This study includes the dynamic analysis in the frequency domain of a cracked plate undergoing forced flexural vibrations in a range of frequencies generated by a pair of piezoelectric actuators. The dynamic analysis in the time domain is also performed for the oscillating structures with piezoelectric strips subjected to mechanical or unsteady aerodynamic loads. It was found that this method is quite effective in detecting cracks in the wing structures subjected to oscillatory aerodynamic loads.

scholarly journals Unsteady Aerodynamic Modeling with Time-Varying Free-Stream Mach Numbers

2006 ◽  
Vol 51 (4) ◽  
pp. 299 ◽  
Author(s):  
Arun I. Jose ◽  
J. Gordon Leishman ◽  
James D. Baeder
Keyword(s):  
Free Stream ◽  
Time Varying ◽  
Aerodynamic Modeling ◽  
Unsteady Aerodynamic ◽  
Mach Numbers

Continuous-Time State-Space Unsteady Aerodynamic Modeling for Efficient Loads Analysis

AIAA Journal ◽  
2018 ◽  
Vol 56 (3) ◽  
pp. 905-916 ◽  
Author(s):  
Noud P. M. Werter ◽  
Roeland De Breuker ◽  
Mostafa M. Abdalla
Keyword(s):  
State Space ◽  
Continuous Time ◽  
Aerodynamic Modeling ◽  
Unsteady Aerodynamic ◽  
Loads Analysis
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