The aeroballistic technique for studying sonic-boom characteristics

被引：0
作者：
V. I. Zvegintsev
A. V. Potapkin
机构：
[1] Khristianovich Institute of Theoretical and Applied Mechanics SB RAS,
来源：
Thermophysics and Aeromechanics | 2018年 / 25卷
关键词：
supersonic flight; sonic boom; far zone; ballistic experiment;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
In the present paper, we analyze a suggestion implying the use of the aeroballistic technique for carrying out studies of shock-wave (sonic-boom) characteristics at large distances from the freely flying model. An analysis of the main engineering solutions ensuring the possibility of implementing the proposed experimental facility in the range of flight velocities of examined models from one to two Mach numbers is performed. A list of scientific and engineering problems pertaining to the study of sonic-boom characteristics in the middle and far zones which can be experimentally tackled with the help of the proposed facility is presented.
引用
收藏
页码：321 / 330
页数：9
相关论文
共 31 条
[1]  
Belov V.E.(1976)Measurement of the sonic–boom char–acteristics by a ballistic method Uchenye Zapiski TsAGI 7 143-146
[2]  
Gur’yashkin L.P.(1985)Parameters of shock waves generated by bodies of revolution in a homogeneous atmosphere Fluid Mechanics Soviet Research 14 31-39
[3]  
Krasil’shchikov A.P.(2001)Controlling the parameters of a shock wave by means of the mass and energy supply Fluid Dynamics 5 136-142
[4]  
Surikova I.M.(1973)Experimental studies of the impact of atmospheric turbulence on the sonic boom Trudy TsAGI 1489 51-74
[5]  
Chirkashenko V.F.(2013)Reduction of the sonic boom level in supersonic aircraft flight by the method of surface cooling Thermophysics and Aeromechanics 20 669-678
[6]  
Yudintsev Yu.N.(2011)Effect of the supersonic transport con–figuration on the sonic boom parameters Thermophysics and Aeromechanics 18 507-522
[7]  
Chirkashenko V.F.(2014)Reduction of the sonic boom level by heating the flow in front of the body Shock Waves 24 429-437
[8]  
Garanin A.F.(2011)Calculation of shock–wave parameters far from origination by combined numerical–analytical methods J. Appl. Mech. Tech. Phys. 52 169-177
[9]  
Tret’yakov P.K.(1983)Numerical solution of the problem of focusing of shock waves generated by a supersonic aircraft Uchenye Zapiski TsAGI 14 26-36
[10]  
Yudintsev Yu.N.(2016)Full–field sonic boom simulation in stratified atmosphere AIAA J. 54 3223-3231
1234