NASA NTRS · 19910000054
Computing The Dynamics Of Helicopters
Abstract
Comprehensive Analytical Model of Rotorcraft Aerodynamics (CAMRAD) computer program designed to calculate performance of, loads on, and noise generated by, helicopter rotor; vibration of helicopter and its response to gusts; dynamics and handling qualities of helicopter in flight; and aeroelastic stability of helicopter as system. Analysis consistent combination of structural, inertial, and aerodynamical mathematical models applicable to wide range of problems and wide class of vehicles. Written in FORTRAN 77.
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Johnson, Wayne. 1991-02-01. Computing The Dynamics Of Helicopters. https://ntrs.nasa.gov/citations/19910000054
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