| タイトル | Support System Effects on the NASA Common Research Model |
| 本文（外部サイト） | http://hdl.handle.net/2060/20120001333 |
| 著者（英） | Rivers, S. Melissa B.; Hunter, Craig A. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2012-01-09 |
| 言語 | eng |
| 内容記述 | An experimental investigation of the NASA Common Research Model was conducted in the NASA Langley National Transonic Facility and NASA Ames 11-Foot Transonic Wind Tunnel Facility for use in the Drag Prediction Workshop. As data from the experimental investigations was collected, a large difference in moment values was seen between the experimental and the computational data from the 4th Drag Prediction Workshop. This difference led to the present work. In this study, a computational assessment has been undertaken to investigate model support system interference effects on the Common Research Model. The configurations computed during this investigation were the wing/body/tail=0deg without the support system and the wing/body/tail=0deg with the support system. The results from this investigation confirm that the addition of the support system to the computational cases does shift the pitching moment in the direction of the experimental results. |
| NASA分類 | Aerodynamics |
| レポートNO | AIAA Paper 2012-0707
NF1676L-12888 |
| 権利 | No Copyright |
