[1] Mahulikar S P, Sonawance H R, Rao G A.Infrared Signature Studies of Aerospace Vehicles[J].Progress in Aerospace Science, 2007,3(7-8):218-245.
[2] 额日其太,王强,陈渭鹏.两种涡扇发动机排气系统红外辐射特性的比较[J].推进技术, 2003,4(4):334-367.(Eriqitai, WANG Qiang, CHEN Wei-peng.Comparative Investigation of the Infrared Characteristics for Two Exhaust Systems of a Turbofan Engine[J].Journal of Propulsion Technology, 2003,4(4):334-336.)
[3] HU Hai-yang, WANG Qiang.A Numerical Simulation on the Infrared Radiation of Hot Exhausting Nozzles with a Coupled Flow and Heat Transfer Mode[J].Science China Technological Sciences, 2010,3(10):2699-2707.
[4] 刘友宏,邵万仁,张锦秀.发动机排气系统及尾喷流的流场和红外特征数值模拟[J].航空动力学报, 2008,3(4):591-597.
[5] 黄伟,吉洪湖,斯仁,等.涡扇发动机排气系统红外特征[J].推进技术, 2010,1(6).(HUANG Wei, JI Hong-hu, SI Ren, et al.Infrared Characteristics Calculating of Turbofan Engine Exhaust System[J].Journal of Propulsion Technology, 2010,1(6).)
[6] ZHU Xi-juan, Eriqitai, LI Xi-xi, et al.Infrared Radiation Simulation of Exhaust System by Coupling FVM with Narrow Band K-Distribution[J].Journal of Aerospace Power, 2012,7(1):25-32.
[7] Nicholas J G, Dennis A Y, William A E.Evaluation of Modified Two-Equation Turbulence Models for Jet Flow Predictions[R].AIAA 2006-490.
[8] Sarkar S, Erlebacher G, Hussaini M Y, et al.The Analysis and Modeling of Dilatational Terms in Compressible Turbulence[J].Journal of Fluid Mechanics, 1991,7:473-495.
[9] Dembowski M A, Georgiadis N J.An Evaluation of Parameters Influencing Jet Mixing Using the WIND Navier-Stokes Code[R].NASA TM-2002-211727.
[10] Engblom W A, Georgiadis N J.Investigation of Variable-Diffusion Turbulence Model Correction for Round Jets[R].AIAA 2005-3085.
[11] Jones W P, Launder B E.The Prediction of Laminarization with a Two-Equation Model of Turbulence[J].Int.J.Heat and Mass Transfer, 1972,5(2):301-314.
[12] 胡海洋,王强.跨声速条件下轴对称收扩喷管内外流场的数值研究[J].航空动力学报, 2008,3(6).
[13] Back L H,Massier P F,Gier H L.Convective Heat Transfer in a Converging-Diverging Nozzle[J].Int.J.Heat and Mass Transfer, 1964,7(11):549-568．
[14] 黄宏艳,王强.轴对称喷管内外流场与结构温度场耦合计算[J].推进技术, 2008,9(2).(HUANG Hong-yan, WANG Qiang.Coupled Numerical Study of Flow Field and Heated Structure for Axisymmetric Nozzles[J].Journal of Propulsion Technology, 2008,9(2).)
[15] Bridges J E, Wernet M P.Measurements of the Aeroacoustic Sound in Hot Jets[R].AIAA 2003-3130.
[16] 朱希娟.基于高精度气体模型的飞行器排气系统红外辐射特性研究[D].北京:北京航空航天大学,2011.
|
