Full-Field Sonic Boom Simulation in Stratified Atmosphere

被引:34
作者
Yamashita, Rei [1 ]
Suzuki, Kojiro [1 ]
机构
[1] Univ Tokyo, Dept Adv Energy, 5-1-5 Kashiwanoha, Kashiwa, Chiba 2778561, Japan
关键词
COMPUTATIONAL METHODS; PREDICTION; EQUATION; SCHEME;
D O I
10.2514/1.J054581
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper discusses the usefulness of a full-field simulation as a sonic boom prediction method, wherein the analysis of the entire flowfield as a single computational domain is presented, including both the near field around a supersonic body and the far field reaching the ground. The three-dimensional Euler equations with a gravity term to create a realistic atmospheric model stratified with altitude are numerically solved by solution-adapted structured grids. Computations are made to reproduce the Drop test for Simplified Evaluation of Non-symmetrically Distributed sonicboom(D-SEND) # 1, conducted by the Japan Aerospace Exploration Agency. As a result, this paper describes the world ' s first successful reproduction by direct flight-test simulation of the evaluation of a sonic boom strength. The computational results clarify the sonic boom propagation, including the three-dimensional structure of the shock wave in the real environmental condition. Moreover, the results of the full-field simulations are in good agreement with those of the waveform parameter method, which is a representative prediction method for sonic booms, and the flight-test data in the D-SEND database provided by the Japan Aerospace Exploration Agency.
引用
收藏
页码:3223 / 3231
页数:9
相关论文
共 33 条
[1]   High-order sonic boom modeling based on adaptive methods [J].
Alauzet, F. ;
Loseille, A. .
JOURNAL OF COMPUTATIONAL PHYSICS, 2010, 229 (03) :561-593
[2]   Multidisciplinary Optimization with Applications to Sonic-Boom Minimization [J].
Alonso, Juan J. ;
Colonno, Michael R. .
ANNUAL REVIEW OF FLUID MECHANICS, VOL 44, 2012, 44 :505-526
[3]  
[Anonymous], D SEND DAT
[4]  
[Anonymous], 1975, 25331975 ISO
[5]  
[Anonymous], 1972, TND6832 NASA
[6]   Numerical simulation of sonic boom focusing [J].
Auger, T ;
Coulouvrat, F .
AIAA JOURNAL, 2002, 40 (09) :1726-1734
[7]  
Darden C. M., 1979, TP1348 NASA
[8]   Lobe Balancing Design Method to Create Frozen Sonic Booms Using Aircraft Components [J].
Jung, Timothy P. ;
Starkey, Ryan P. ;
Argrow, Brian .
JOURNAL OF AIRCRAFT, 2012, 49 (06) :1878-1893
[9]  
KANDIL O, 2002, 20022542 AIAA
[10]  
Kandil O. A., 2005, 20050013 AIAA, DOI [10.2514/6.2005-13, DOI 10.2514/6.2005-13]