@inproceedings{a3b1b93c6dc642ac8907e424d8e904a8,
title = "One-dimensional impulse analysis on the scramjet combustor",
abstract = "Quantitative data obtained in the scramjet experiments are generally limited to wall static pressure distributions. To aid interpretation of the experimental results, a one dimensional analysis code was required. In present paper, a modification on the area of supersonic core flow was introduced based on two scramjet combustor configurations with cavity and strut, respectively. By substituting measured wall static pressure, other important parameters of the flow field in the combustor were obtained. By comparing with the 3-dimensional numerical simulation and experimental exit total pressure profiles, the validation of the modification method and analysis code was testified.",
author = "Zhao Yongsheng and Lin Yuzhen and Wang Jianchen and Liu Wei and Zhang Yan",
note = "Publisher Copyright: {\textcopyright} 2014 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.; 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014 ; Conference date: 28-07-2014 Through 30-07-2014",
year = "2014",
doi = "10.2514/6.2014-3666",
language = "英语",
series = "50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014",
}