| Citation: | Effect of flow capture shape on the geometry and aerodynamic characteristics for inward turning inlet's external compression segment[J]. Journal of Aerospace Power, 2017, 32(4): 890-899. doi: 10.13224/j.cnki.jasp.2017.04.014 |
| [1] |
Bulman M J,Siebenhaar A.The rebirth of round hypersonic propulsion[R].AIAA-2006-5035,2006.
|
| [2] |
Barkmeyer D E,Starkey R P,Lewis M J.Inverse waverider design for inward turning inlets[R].AIAA-2005-3915, 2005.
|
| [3] |
Jacobsen L S,Tam C J,Behdadnia R,et al.Starting and operation of a streamline-traced busemann inlet at Mach 4[R].AIAA-2006-4508,2006.
|
| [4] |
Ungewitter R J,Ott J D,Dash S M.Advanced modeling methods for hypersonic scramjet evaluation[R].AIAA-2006-4578,2006.
|
| [5] |
Matthews A J,Jones T V.Design and test of a modular waverider hypersonic intake[R].AIAA-2005-3379,2005.
|
| [6] |
李永洲,张堃元,南向军.基于马赫数分布规律可控概念的高超声速内收缩进气道设计[J].航空动力学报,2012,27(11):2484-2491.LI Yongzhou,ZHANG Kunyuan,NAN Xiangjun.Design of hypersonic inward turning inlets base on concept of controllable Mach number distribution[J].Journal of Aerospace Power,2012,27(11):2484-2491.(in Chinese)
|
| [7] |
Molder S,Szpiro J.Busemman inlet for hypersonic speeds [J].Journal of Spacecraft and Rockets,1966,3(8):1303-1304.
|
| [8] |
Molder S.Internal,axisymmetric,conical flow[J].AIAA Journal,1967,5(7):1252-1255.
|
| [9] |
Molder S,Dsouza N.Applicability of hypersonic small-disturbance theory and similitude to internal hyper-sonic conical flows[J].Journal of Spacecraft and Rockets,1970,7(2):149-154.
|
| [10] |
Smart M K.Design of three-dimensional hypersonic inlets with rectangular-to-elliptical shape transition[J].Journal of Propulsion and Power,1999,15(3):408-416.
|
| [11] |
Smart M K.Experimental testing of a hypersonic inlet with rectangular-to-elliptical shape transition[J].Journal of Propulsion and Power,2001,17(2):276-283.
|
| [12] |
Smart M K,White J A.Computational investigation of the performance and back-pressure limits of a hypersonic inlet[R].AIAA-2002-0508,2002.
|
| [13] |
Malo-Molina F J,Gaitonde D V,Kutschenreuter P H.Numerical investigation of an innovative inward turning inlet[R].AIAA 2005-4871,2005.
|
| [14] |
Malo-Molina F J,Gaitonde D V,Ebrahimi H B,et al.Analysis of an innovative inward turning inlet using an Air-JP8 combustion mixture at Mach 7[R].AIAA-2006-3041,2006.
|
| [15] |
尤延铖,梁德旺,黄国平.一种新型内乘波式进气道初步研究[J].推进技术,2006,27(3):252-256.YOU Yancheng,LIANG Dewang,HUANG Guoping.Investigation of internal waverider-derived hypersonic inlet[J].Journal of Propulsion Technology,2006,27(3):252-256.(in Chinese)
|
| [16] |
尤延铖,梁德旺.内乘波式进气道内收缩基本流场研究[J].空气动力学学报,2008,26(2):203-207.YOU Yancheng,LIANG Dewang.Investigation of internal compression flowfield for internal waverider-derived inlet[J].Acta Aerodynamica Sinica,2008,26(2):203-207.(in Chinese)
|
| [17] |
南向军,张堃元,金志光,等.压升规律可控的高超声速内收缩进气道设计[J].航空动力学报,2011,26(3):518-523.NAN Xiangjun,ZHANG Kunyuan,JIN Zhiguang,et al.Investigation on hypersonic inward turning inlets with controlled pressure gradient[J].Journal of Aerospace Power,2011,26(3):518-523.(in Chinese)
|
| [18] |
南向军,张堃元,金志光.基于反正切曲线压升规律设计高超内收缩进气道[J].航空动力学报,2011,26(11):2571-2577.NAN Xiangjun,ZHANG Kunyuan,JIN Zhiguang.Design of hypersonic inward turning inlets with basic flowfield using arc tangent curve law of pressure rise[J].Journal of Aerospace Power,2011,26(11):2571-2577.(in Chinese)
|
| [19] |
李永洲,张堃元,王磊,等.马赫数分布可控的基准流场灵敏度分析与优化设计[J].航空动力学报,2013,28(4):765-774.LI Yongzhou,ZHANG Kunyuan,WANG Lei,et al.Sensitivity analysis and optimization design of basic flowfield with controllable Mach number distribution [J].Journal of Aerospace Power,2013,28(4):765-774.(in Chinese)
|
| [20] |
左克罗,霍夫曼.气体动力学[M].北京:国防工业出版社,1984.
|
| [21] |
Taha A A,Tiwari S N,Mohieldin T O.Validation of fluent CFD code in supersonic flow fields[R].AIAA-2001-2637,2001.
|
| [22] |
Koutsavdis E,Stuckert G.Numerical investigation of the flow characteristic of plug nozzles using fluent[R].AIAA-2002-0511,2002.
|
| [23] |
Allamaprabhu C,Raghunandan B,Morinigo J.Improved prediction of flow separation in thrust optimized parabolic nozzles with fluent[R].AIAA-2011-5689,2011.
|