Helicopter rotor blade design for minimum vibration
By: Robert B. Taylor
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; United Technologies Research Center; Aeromechanics Laboratory
Series: NASA contractor report -- 3825; AVSCOM technical report -- 84-A-2
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1984
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 127
Subjects: Rotors (Helicopters); Stability of helicopters
Notes: "United Technologies Research Center."

Distributed to depository libraries in microfiche

"October 1984"--Cover

STAR category 05

Includes bibliographical references

Final report

Aeromechanics Laboratory, U.S. Army Research and Technology Laboratories, Ames Research Center. NAS2-11025