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A high fidelity real-time simulation of a small turboshaft engine
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ballin, Mark G. |
| Copyright Year | 1988 |
| Description | A high-fidelity component-type model and real-time digital simulation of the General Electric T700-GE-700 turboshaft engine were developed for use with current generation real-time blade-element rotor helicopter simulations. A control system model based on the specification fuel control system used in the UH-60A Black Hawk helicopter is also presented. The modeling assumptions and real-time digital implementation methods particular to the simulation of small turboshaft engines are described. The validity of the simulation is demonstrated by comparison with analysis-oriented simulations developed by the manufacturer, available test data, and flight-test time histories. |
| File Size | 3028321 |
| Page Count | 104 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19880016994 |
| Archival Resource Key | ark:/13960/t3mw7b44p |
| Language | English |
| Publisher Date | 1988-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Control Systems Design Helicopters Digital Simulation Turboshafts Models Rotor Blades Turbine Engines Flight Simulation Real Time Operation Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |