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Propulsion airframe integration test techniques for hypersonic airbreathing configurations at nasa langley research center
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Huebner, Lawrence D. Andrews Jr., Earl H. Witte, David W. Cabell, Karen F. Trexler, Carl A. |
| Copyright Year | 2003 |
| Description | The scope and significance of propulsion airframe integration (PAI) for hypersonic airbreathing vehicles is presented through a discussion of the PAI test techniques utilized at NASA Langley Research Center. Four primary types of PAI model tests utilized at NASA Langley for hypersonic airbreathing vehicles are discussed. The four types of PAI test models examined are the forebody/inlet test model, the partial-width/truncated propulsion flowpath test model, the powered exhaust simulation test model, and the full-length/width propulsion flowpath test model. The test technique for each of these four types of PAI test models is described, and the relevant PAI issues addressed by each test technique are illustrated through the presentation of recent PAI test data. |
| File Size | 2274628 |
| Page Count | 22 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20040000798 |
| Archival Resource Key | ark:/13960/t3xt0nz91 |
| Language | English |
| Publisher Date | 2003-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Measure and Integration Aerodynamic Configurations Engine Airframe Integration Air Breathing Engines Forebodies Hypersonic Vehicles Powered Models Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
