ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2023, Vol. 44 ›› Issue (2): 626952-626952.doi: 10.7527/S1000-6893.2022.26952
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Zhongchen LIU1,2,3, Zhansen QIAN1,2,3(), Xuefei LI1,2,3, Yan LENG1,2,3, Dapeng GUO1,3
Received:
2022-01-14
Revised:
2022-02-25
Accepted:
2022-03-14
Online:
2023-01-25
Published:
2022-03-22
Contact:
Zhansen QIAN
E-mail:qianzs@avicari.com.cn
Supported by:
CLC Number:
Zhongchen LIU, Zhansen QIAN, Xuefei LI, Yan LENG, Dapeng GUO. Wind tunnel test techniques for exhaust nozzle plume effects on near-field sonic boom[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 626952-626952.
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All copyright © editorial office of Chinese Journal of Aeronautics
Total visits: 6658907 Today visits: 1341