Aeorelastic analysis for helicopter rotor blades with time-variable, nonlinear structural twist and multiple structural redundancy-mathematical derivation and program user's manual
By: Richard L. Bielawa.
Contributors: U.S. Army Air Mobility Research and Development Laboratory.; Langley Research Center.; United States. National Aeronautics and Space Administration.; United Technologies Research Center.
Series: NASA contractor report ; NASA CR-2638; NASA contractor report -- NASA CR-2638.
Publisher: National Aeronautics and Space Administration; for sale by the National Technical Information Service
Published: 1976
Place of publication: Washington; Springfield, Va
Language: eng
Number of pages: 150
Subjects: Rotors (Helicopters) -- Aerodynamics.; Aeroelasticity -- Mathematical models.; Composite materials -- Analysis.; Equations of motion.
Notes: Cover title.

Prepared under Contract no. NAS.1-10960 by United Technologies Research Center, East Hartford, Conn. for Langley Research Center and U.S. Army Air Mobility R & D Laboratory.

Bibliography: p. 89-90.