Aeroelastic effects in multirotor vehicles
Subtitle: Part II: Methods of solution and results illustrating coupled rotor/body aeromechanical stability
By: prepared for Ames Research Center.
Contributors: Friedmann, Peretz P.; Ames Research Center; University of California. Mechanical, Aerospace and Nuclear Engineering Dept
Publisher: Ames Research Center
Published: 1987
Place of publication: Moffett Field, Calif
Number of pages: 159
Subjects: Aeroelasticity; Rotary wing aircraft; Stability
Notes: Bibliographical references: p.125.