The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover/

Main Author: Bousman, William G.
Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Division, Ames Research Center, United States. Army Aviation Research and Technology Activity, United States. National Aeronautics and Space Administration., Scientific and Technical Information Division
Format: Book
Language:English
Published: Washington: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1990
Series:NASA technical paper AVSCOM technical report 3002
Subjects:
ΒιβλιοθήκηΤαξιθετικός αριθμόςΑριθμός ΑντιτύπωνΠληροφορίεςΚατάσταση
Δημοκρίτειο Πανεπιστήμιο ΘράκηςTL 521 .31ΠροβολήOPAC