Vibration reduction in helicopter rotors using an actively controlled partial span trailing edge flap located on the blade
By: prepared for Ames Research Center.
Contributors: Friedmann, Peretz P.; Ames Research Center
Publisher: Ames Research Center
Published: 1994
Place of publication: Moffett Field, Calif
Number of pages: 398
Subjects: Helicopters; Rotary wings; Vibration
Notes: Includes bibliographical references: p. 204-207.