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Real-time simulation of aeroheating of the hyper-x airplane
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Gong Sr., Les |
| Copyright Year | 2005 |
| Description | A capability for real-time computational simulation of aeroheating has been developed in support of the Hyper-X program, which is directed toward demonstrating the feasibility of operating an air-breathing ramjet/scramjet engine at mach 5, mach 7, and mach 10. The simulation software will serve as a valuable design tool for initial trajectory studies in which aerodynamic heating is expected to exert a major influence in the design of the Hyper-X airplane; this tool will aid in the selection of materials, sizing of structural skin thicknesses, and selection of components of a thermal-protection system (TPS) for structures that must be insulated against aeroheating. |
| File Size | 87951 |
| Page Count | 1 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20110014692 |
| Archival Resource Key | ark:/13960/t1wd8tn93 |
| Language | English |
| Publisher Date | 2005-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Structural Design Ramjet Engines Hypersonic Speed Thermal Protection Supersonic Combustion Ramjet Engines Aerodynamic Heating Air Breathing Engines Flight Test Vehicles Computerized Simulation Hypersonic Aircraft Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
