Effect of structural flexibility on the design of vibration-isolating mounts for aircraft engines
By: William H. Phillips
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Series: NASA technical memorandum -- 85725
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; For sale by the National Technical Information Service]
Published: 1984
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 21
Subjects: Airplanes -- Motors -- Design and construction
Notes: Distributed to depository libraries in microfiche

"February 1984"--Cover

Subject category 39

Includes bibliographical references