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Untersuchung der Flugdynamik eines Tragschraubers im Seitengleitflug

Sachs, Falk (2013) Untersuchung der Flugdynamik eines Tragschraubers im Seitengleitflug. Diploma. DLR-Interner Bericht. DLR-IB 111-2013/59, 122 S.

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A gyrocopter is a rotary wing vehicle, which constantly flies with its rotor in autorotative state. The design of the plane is very asymmetric. This is due to flight mechanical effects arising in flight conditions. A very important influence on flight dynamics is caused by the flapping of the rotorblades. The gyrocopter allows extreme sideslip angels and consequently steep approaches. Those manoeuvres have been suspected to be a possible cause for several accidents. This work focuses on effects on flight mechanics caused by sideslip manoeuvres and explains influences on flapping and stability in sideslip condition. The results were obtained by flight tests as well as simulations with a validated gyrocopter Simulink-model.

Item URL in elib:https://elib.dlr.de/88528/
Document Type:Monograph (DLR-Interner Bericht, Diploma)
Title:Untersuchung der Flugdynamik eines Tragschraubers im Seitengleitflug
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Date:19 April 2013
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In ISI Web of Science:No
Number of Pages:122
Keywords:Schlagwinkel, Gyrocopter, Tragschrauber, Seitengleitflug, Sideslip, Autorotation
Institution:TU Braunschweig
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L - no assignment
DLR - Research theme (Project):L - no assignment (old)
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Flight Dynamics and Simulation
Deposited By: Sachs, Falk
Deposited On:07 Apr 2014 15:04
Last Modified:31 Jul 2019 19:45

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