Investigation on Hypersonic Inlet Starting Process in Continuous Freejet Wind Tunnel
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Bibliographic record
Abstract
No AccessTechnical NoteInvestigation on Hypersonic Inlet Starting Process in Continuous Freejet Wind TunnelYi Wang, Zhenguo Wang, Jianhan Liang and Xiaoqiang FanYi WangScience and Technology on Scramjet Laboratory, National University of Defense Technology, 410073 Changsha, People's Republic of China, Zhenguo WangScience and Technology on Scramjet Laboratory, National University of Defense Technology, 410073 Changsha, People's Republic of China, Jianhan LiangScience and Technology on Scramjet Laboratory, National University of Defense Technology, 410073 Changsha, People's Republic of China and Xiaoqiang FanScience and Technology on Scramjet Laboratory, National University of Defense Technology, 410073 Changsha, People's Republic of ChinaPublished Online:20 Oct 2014https://doi.org/10.2514/1.B35289SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations About References [1] Mahoney J., Inlets for Supersonic Missiles, AIAA Education Series, AIAA, New York, 1990, p. 1. Google Scholar[2] Curran E. and Murthy S., Scramjet Propulsion, Vol. 189, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 2000, p. 449. Google Scholar[3] Van Wie D., Kwok F. and Walsh R., "Starting Characteristics of Supersonic Inlets," AIAA Paper 1996-2914, 1996. LinkGoogle Scholar[4] Hawkins W. and Marquart E., "Two-Dimensional Generic Inlet Unstart Detection at Mach 2.5–5.0," AIAA Paper 1995-6019, 1995. LinkGoogle Scholar[5] Vinogradov V., Stepanov V. and Goldfeld M., "Experimental and Numerical Investigation of Two Concepts of the Hypersonic Inlet," AIAA Paper 1995-2721, 1995. LinkGoogle Scholar[6] Smart M., Trexler C. and Goldman A., "A Combined Experimental/Computational Investigation of Rocket Based Combined Cycle Inlet," AIAA Paper 2001-0671, 2011. Google Scholar[7] Wagner J., Valdivia A., Yuceil K., Clemens N. T. and Dolling D. S., "An Experimental Investigation of Supersonic Inlet Unstart," AIAA Paper 2007-4352, 2007. LinkGoogle Scholar[8] Falempin F., Wendling E., Goldfeld M., Starov A. and Timofeev K., "Influence of Gas Injection and Combustion on Start and Characteristics of Inlet," AIAA Paper 2008-2514, 2008. LinkGoogle Scholar[9] Lu F. and Marren D., Advanced Hypersonic Test Facilities, Vol. 198, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 2002, p. 24. Google Scholar[10] McGregor R., Molder S. and Paisley T., "Hypersonic Inlet Flow Starting in the Gun Tunnel," Investigation in the Fluid Dynamics of Scramjet Inlets, Ryerson Polytechnical Inst. and Univ. of Toronto, Canada, July 1992. Google Scholar[11] Fan X., "Design Method, Numerical Simulation and Experimental Research of Hypersonic Inlet," Ph.D. Thesis, National Univ. of Defense Technology, Changsha, PRC, 2006, pp. 79–81 (in Chinese). Google Scholar[12] Voland R., Rock K., Huebner L., Witte D. W., Fischer K. E. and McClinton C. R., "Hyper-X Engine Design and Ground Test Program," AIAA Paper 1998-1532, 1998. LinkGoogle Scholar[13] Wang Y., Liang J., Fan X., Liu W. and Wang Z., "Investigation on the Unstarted Flowfield of a Three-Dimensional Sidewall Compression Hypersonic Inlet," AIAA Paper 2009-7404, 2009. Google Scholar Previous article Next article
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Full frame distilled prediction
Teacher imitationNot calibrated prevalence, not ground truth. Human validation pending. Learned from the 10,348 direct Codex labels and 10,348 direct Gemma labels. Candidate is the union of thresholded teacher heads; consensus is their intersection. These outputs are machine_predicted_unvalidated and are not human labels or direct frontier model labels.
Codex and Gemma teacher scores by category
| Category | Codex | Gemma |
|---|---|---|
| Metaresearch | 0.000 | 0.000 |
| Meta-epidemiology (narrow) | 0.000 | 0.000 |
| Meta-epidemiology (broad) | 0.000 | 0.000 |
| Bibliometrics | 0.000 | 0.000 |
| Science and technology studies | 0.000 | 0.000 |
| Scholarly communication | 0.000 | 0.000 |
| Open science | 0.000 | 0.000 |
| Research integrity | 0.000 | 0.000 |
| Insufficient payload (model declined to judge) | 0.000 | 0.000 |
Machine scores (provisional)
The two teacher heads of the student model, read on this work. A score orders the frame for review; it never asserts a category, and the validation status ships verbatim with every row.
Baseline scores from an immature model (maturity gate not passed, 7 training rounds). Scores rank; they never assert a category.
score_only:v0-immature-baseline · verbatim from the scoring run: score_only means the number may rank works, and no category label ships from it