A study was conducted to establish a coupled rotor/propulsion analysis that would be applicable to a wide range of rotorcraft systems. The effort included the following tasks: (1) development of a model structure suitable for simulating a wide range of rotorcraft configurations; (2) defined a methodology for parameterizing the model structure to represent a particular rotorcraft; (3) constructing a nonlinear coupled rotor/propulsion model as a test case to use in analyzing coupled system dynamics; and (4) an attempt to develop a mostly linear coupled model derived from the complete nonlinear simulations. Documentation of the computer models developed is presented.
Development of a rotorcraft. Propulsion dynamics interface analysis, volume 2
1982-08-01
Report
No indication
English
Springer Verlag | 2023
|High-speed rotorcraft propulsion
NTRS | 1991
|ADVERTISERS - Rotorcraft Propulsion Meeting
Online Contents | 1999