TY - JOUR
T1 - 声爆研究的现状与挑战
AU - Qian, Zhansen
AU - Han, Zhonghua
N1 - Publisher Copyright:
© 2019, The Editorial Board of Acta Aerodynamica Sinica. All right reserved.
PY - 2019/8/1
Y1 - 2019/8/1
N2 - Sonic boom is a special aero-acoustic phenomenon for supersonic aircraft, which contains both the fields of aerodynamics and nonlinear acoustics, so it is of important academic significance and application prospect. The present paper introduces its basic conception and major characteristics, the research history of its generation, development and evolution, and its harmfulness; Then the numerical simulation method, wind tunnel experiment method and flight test method of sonic boom researches are emphatically presented, and also including the recently proposed sonic boom inhibition and low boom optimization design methods; Finally, the current technique difficulties and challenges of sonic boom prediction are summarized.
AB - Sonic boom is a special aero-acoustic phenomenon for supersonic aircraft, which contains both the fields of aerodynamics and nonlinear acoustics, so it is of important academic significance and application prospect. The present paper introduces its basic conception and major characteristics, the research history of its generation, development and evolution, and its harmfulness; Then the numerical simulation method, wind tunnel experiment method and flight test method of sonic boom researches are emphatically presented, and also including the recently proposed sonic boom inhibition and low boom optimization design methods; Finally, the current technique difficulties and challenges of sonic boom prediction are summarized.
KW - Harmfulness of sonic boom
KW - Inhibition of sonic boom
KW - Low boom design
KW - Numerical prediction
KW - Sonic boom
KW - Spatial pressure
KW - Wind tunnel test
UR - http://www.scopus.com/inward/record.url?scp=85072182622&partnerID=8YFLogxK
U2 - 10.7638/kqdlxxb-2019.0054
DO - 10.7638/kqdlxxb-2019.0054
M3 - 文章
AN - SCOPUS:85072182622
SN - 0258-1825
VL - 37
SP - 601
EP - 619
JO - Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica
JF - Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica
IS - 4
ER -