Wind-tunnel investigation of the effects of blade tip geometry on the interaction of torsional loads and performance for an articulated helicopter rotor/

Main Author: Yeager, William T.
Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Branch, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Army Research and Technology Laboratories U.S. Structures Laboratory, Langley Research Center
Other Authors: Mantay, Wayne R.
Format: Book
Language:English
Published: Washington: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1981
Series:NASA technical paper AVRADCOM technical report 1926
Subjects:
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100 1 |a Yeager, William T. 
245 1 0 |a Wind-tunnel investigation of the effects of blade tip geometry on the interaction of torsional loads and performance for an articulated helicopter rotor/  |c William T. Yeager, Jr., and Wayne R. Mantay 
260 |a Washington:  |b National Aeronautics and Space Administration, Scientific and Technical Information Branch,  |c 1981 
300 |a 62 σ. :  |b εικ. ;  |c 28 εκ. 
490 0 |a NASA technical paper  |v 1926  |a AVRADCOM technical report 
504 |a Περιέχει βιβλιογραφικές παραπομπές  |v 81-B-5 
650 0 |a Rotors (Helicopters)  |x Aerodynamics 
700 1 |a Mantay, Wayne R. 
710 |a United States  |b National Aeronautics and Space Administration  |b Scientific and Technical Information Branch 
710 0 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Branch 
710 0 |a Army Research and Technology Laboratories U.S.  |b Structures Laboratory 
710 2 |a Langley Research Center 
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