Flexible aircraft gust encounter simulation using subspace projection model reduction-Reference-Cited by-同舟云学术

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Flexible aircraft gust encounter simulation using subspace projection model reduction

Published:2019-03 Issue: Volume:86 Page:805-817
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Bekemeyer P.,Timme S.

Funder

Innovate UK

UK's innovation agency

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference66 articles.

1. A doublet lattice method for calculating lift distribution on oscillating surfaces in subsonic flow;Albano;AIAA J.,1969

2. Sears function and lifting surface theory for harmonic gust fields;Giesing;J. Aircr.,1970

3. Comparison of unsteady aerodynamic modelling methodologies with respect to flight loads analysis;Kier,2005

4. DLM-correction methods for aerodynamic gust response prediction;Dimitrov,2013

5. CFD-based models of aerodynamic gust response;Raveh;J. Aircr.,2007

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1. Development of a Novel Small-Scale Gust Generator Research Facility;Aerospace;2024-01-19

2. Global stability analysis of elastic aircraft in edge-of-the-envelope flow;Journal of Fluid Mechanics;2023-07-12

3. Nonlinear Low-Dimensional Model Order Reduction with Subspace Interpolation for Gust Applications with the Linear Frequency Domain Approach;AIAA AVIATION 2023 Forum;2023-06-08

4. Gusts Encountered by Flying Vehicles in Proximity to Buildings;Drones;2022-12-28

5. Aerodynamic Response of a Serpentine Inlet to Horizontal Periodic Gusts;Aerospace;2022-12-14

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