The effects of nonuniform swash-plate stiffness on coupled blade-control system dynamics and stability.
Part II,
Computer program listing /
by Vincent J. Piarulli.

Description

Main Author: Piarulli, Vincent J.
Related Names: Langley Research Center.
Rochester Applied Science Associates, inc.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration ; 1971.
Subjects: Vibration mode.
Stability.
Matrices (mathematics).
Laplace transformation.
Rotary wings.
Helicopters.
Flexible bodies.
Dynamic response.
Computer programs.
Summary: This report investigates a computer program for calculating effects of swash-plate stiffness on helicopter rotor system dynamics and stability.
Note: "NASA CR-1818."
"August 1971."
Cover title.
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 02/03/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19710023321%5f1971023321.pdf.
Physical Description: iv, 68 p. : ill. ; 27 cm.
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