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A turbine based combined cycle engine inlet model and mode transition simulation based on hitecc tool (Document No: 20120018037)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Csank, Jeffrey Stueber Sr., Thomas |
| Copyright Year | 2012 |
| Description | An inlet system is being tested to evaluate methodologies for a turbine based combined cycle propulsion system to perform a controlled inlet mode transition. Prior to wind tunnel based hardware testing of controlled mode transitions, simulation models are used to test, debug, and validate potential control algorithms. One candidate simulation package for this purpose is the High Mach Transient Engine Cycle Code (HiTECC). The HiTECC simulation package models the inlet system, propulsion systems, thermal energy, geometry, nozzle, and fuel systems. This paper discusses the modification and redesign of the simulation package and control system to represent the NASA large-scale inlet model for Combined Cycle Engine mode transition studies, mounted in NASA Glenn s 10-foot by 10-foot Supersonic Wind Tunnel. This model will be used for designing and testing candidate control algorithms before implementation. |
| File Size | 2273595 |
| Page Count | 35 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20120018037 |
| Archival Resource Key | ark:/13960/t9j43rk6c |
| Language | English |
| Publisher Date | 2012-07-29 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Propulsion System Performance Engine Inlets Wind Tunnel Tests Computerized Simulation Intake Systems Propulsion System Configurations Thermal Energy Turbine Engines Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Presentation |
