Effect of structural flexibility on the design of vibration-isolating mounts for aircraft engines /
William H. Phillips.

APA Citation

Phillips, W. H., United States. National Aeronautics and Space Administration. Scientific and Technical Information Office. (1984). Effect of structural flexibility on the design of vibration-isolating mounts for aircraft engines. Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Office .

MLA Citation

Phillips, William H, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office. Effect of Structural Flexibility On the Design of Vibration-isolating Mounts for Aircraft Engines. Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Office , 1984.