| タイトル | Propulsion Airframe Integration Test Techniques for Hypersonic Airbreathing Configurations at NASA Langley Research Center |
| 本文（外部サイト） | http://hdl.handle.net/2060/20040000798 |
| 著者（英） | Andrews, Earl H., Jr.; Trexler, Carl A.; Witte, David W.; Cabell, Karen F.; Huebner, Lawrence D. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2003-01-01 |
| 言語 | eng |
| 内容記述 | 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. |
| NASA分類 | Aircraft Design, Testing and Performance |
| レポートNO | AIAA Paper 2003-4406 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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