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Development of a rotorcraft. propulsion dynamics interface analysis, volume 2
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hull, R. |
| Copyright Year | 1982 |
| Description | 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. |
| File Size | 1137777 |
| Page Count | 58 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19820024493 |
| Archival Resource Key | ark:/13960/t4jm73b1x |
| Language | English |
| Publisher Date | 1982-08-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Tables Data Engine Airframe Integration Rotor Aerodynamics Aerodynamic Coefficients Rotary Wing Aircraft Aircraft Configurations Propulsion System Configurations Computer Aided Design User Manuals Computer Programs Matrices Mathematics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
