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Titel:

Flight Testing of a Coaxial Ultralight Rotorcraft

Dokumenttyp:
Konferenzbeitrag
Autor(en):
Feil, R., Rinker, M., Hajek, M.
Abstract:
The results of a full-scale flight test on an ultralight counter-rotating coaxial rotorcraft, the CoAX 2D, are presented. The CoAX 2D was developed and manufactured by edm-aerotec in Geisleden, Germany. It can be operated up to a maximum take-off weight of 450 kg. The helicopter features 2-bladed, 6.5 m diameter upper and lower rotors in teeter configuration with uniform airfoil sections and linearly twisted blades. Fundamental measurements included air data, data from an inertial measurement un...     »
Dewey-Dezimalklassifikation:
620 Ingenieurwissenschaften
Kongress- / Buchtitel:
American Helicopter Society 73rd Annual Forum
Ausrichter der Konferenz:
American Helicopter Society
Publikationsdatum:
10.05.2017
Jahr:
2017
Seiten:
14
Nachgewiesen in:
Scopus
Reviewed:
nein
Sprache:
en
TUM Einrichtung:
Lehrstuhl für Hubschraubertechnologie
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