User: Guest  Login
Title:

Flight Testing of a Coaxial Ultralight Rotorcraft

Document type:
Konferenzbeitrag
Author(s):
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 Decimal Classification:
620 Ingenieurwissenschaften
Book / Congress title:
American Helicopter Society 73rd Annual Forum
Organization:
American Helicopter Society
Date of publication:
10.05.2017
Year:
2017
Pages:
14
Covered by:
Scopus
Reviewed:
nein
Language:
en
TUM Institution:
Lehrstuhl für Hubschraubertechnologie
 BibTeX