APA (7th ed.) Citation

Bousman, W. G., Ames Research Center, & United States. Army Aviation Research and Technology Activity. (1990). The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division.

Chicago Style (17th ed.) Citation

Bousman, William G., Ames Research Center, and United States. Army Aviation Research and Technology Activity. The Effects of Structural Flap-lag and Pitch-lag Coupling on Soft Inplane Hingeless Rotor Stability in Hover. Washington, D.C. : [Springfield, Va.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

MLA (8th ed.) Citation

Bousman, William G., et al. The Effects of Structural Flap-lag and Pitch-lag Coupling on Soft Inplane Hingeless Rotor Stability in Hover. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.