| タイトル | Advanced Concept Studies for Supersonic Commercial Transports Entering Service in the 2018 to 2020 Period |
| 本文（外部サイト） | http://hdl.handle.net/2060/20130010174 |
| 著者（英） | Morgenstern, John; Sokhey, Jack; Norstrud, Nicole; Martens, Steve; Alonso, Juan J. |
| 著者所属（英） | Lockheed Martin Aeronautics Co. |
| 発行日 | 2013-02-01 |
| 言語 | eng |
| 内容記述 | Lockheed Martin Aeronautics Company (LM), working in conjunction with General Electric Global Research (GE GR), Rolls-Royce Liberty Works (RRLW), and Stanford University, herein presents results from the "N+2 Supersonic Validations" contract s initial 22 month phase, addressing the NASA solicitation "Advanced Concept Studies for Supersonic Commercial Transports Entering Service in the 2018 to 2020 Period." This report version adds documentation of an additional three month low boom test task. The key technical objective of this effort was to validate integrated airframe and propulsion technologies and design methodologies. These capabilities aspired to produce a viable supersonic vehicle design with environmental and performance characteristics. Supersonic testing of both airframe and propulsion technologies (including LM3: 97-023 low boom testing and April-June nozzle acoustic testing) verified LM s supersonic low-boom design methodologies and both GE and RRLW's nozzle technologies for future implementation. The N+2 program is aligned with NASA s Supersonic Project and is focused on providing system-level solutions capable of overcoming the environmental and performance/efficiency barriers to practical supersonic flight. NASA proposed "Initial Environmental Targets and Performance Goals for Future Supersonic Civil Aircraft". The LM N+2 studies are built upon LM s prior N+3 100 passenger design studies. The LM N+2 program addresses low boom design and methodology validations with wind tunnel testing, performance and efficiency goals with system level analysis, and low noise validations with two nozzle (GE and RRLW) acoustic tests. |
| NASA分類 | Aircraft Design, Testing and Performance |
| レポートNO | E-18569
PMF-01766
NASA/CR-2013-217820 |
| 権利 | Copyright, Distribution under U.S. Government purpose rights |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/238989 |
