Analysis of supersonic stall bending flutter in axial-flow compressor by actuator disk theory/

Main Author: Adamczyk, John J.
Corporate Authors: United States National Aeronautics and Space Administration Scientific and Technical Information Office, Lewis Research Center, United States. National Aeronautics and Space Administration., Scientific and Technical Information Office
Format: Book
Language:English
Published: Washington: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978
Series:NASA technical paper 1345
Subjects:
ΒιβλιοθήκηΤαξιθετικός αριθμόςΑριθμός ΑντιτύπωνΠληροφορίεςΚατάσταση
Δημοκρίτειο Πανεπιστήμιο ΘράκηςTL 521 .31ΠροβολήOPAC