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Gust loads analysis on a civil transport airliner

Lebkuchen, Hermann Luis (2015) Gust loads analysis on a civil transport airliner. DLR-Interner Bericht. DLR IB 232-2015 J 12. DLR. 66 S.

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In the report, a comparison of gust loads analysis using the classical quasi-static Pratt gust approach, a fully dynamic approach and a Pratt-revised gust formula is undertaken. The evaluation has been performed for a one-degree-of-freedom rigid wing (to reflect and verify Pratt's assumptions in his classical gust definition) as well as for a fully elastic transport air-craft, the so-called DLR D150 configuration. In addition, a comparison has been carried out between the certification specifications CS-23 and CS-25 proposed by the European Aviation Safety Agency (EASA) to calculate gust loads on the aircraft structure. The CS-23 requires only the Pratt's quasi-static method while CS-25 requires the dynamic method for a range of gusts, flight and mass cases. For the analyses, the quasi-static and dynamic methods were implemented in MSC.Nastran, observing the flight envelopes required by the certification specifications.

Item URL in elib:https://elib.dlr.de/127268/
Document Type:Monograph (DLR-Interner Bericht)
Title:Gust loads analysis on a civil transport airliner
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Lebkuchen, Hermann LuisDLRUNSPECIFIED
Date:October 2015
Refereed publication:No
Gold Open Access:No
In ISI Web of Science:No
Number of Pages:66
Keywords:gust loads, loads analysis
Department:Institut für Aeroelastik
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics (old)
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Deposited By: Krüger, Prof. Dr.-Ing. Wolf R.
Deposited On:17 May 2019 11:33
Last Modified:17 May 2019 11:33

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