Rotorcraft blade mode damping identification from random responses using a recursive maximum likelihood algorithm
By: John A. Molusis ; prepared for NASA Langley Research Center and Structures Laboratory, AVRADCOM Research and Technology Laboratories
Contributors: Langley Research Center; Army Research and Technology Laboratories (U.S.). Structures Laboratory; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA contractor report -- 3600
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1982
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 46
Subjects: Rotors (Helicopters)
Notes: "September 1982."

Includes bibliographical references