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FOURIER REGULARIZATION FOR DETERMINING SURFACE HEAT FLUX FROM INTERIOR OBSERVATION BASED ON A SIDEWAYS PARABOLIC EQUATION 被引量:1
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作者 傅初黎 熊向团 李洪芳 《Numerical Mathematics A Journal of Chinese Universities(English Series)》 SCIE 2005年第3期208-216,共9页
In this paper we consider a non-standard inverse heat conduction problem for determining surface heat flux from an interior observation which appears in some applied subjects. This problem is ill-posed in the sense th... In this paper we consider a non-standard inverse heat conduction problem for determining surface heat flux from an interior observation which appears in some applied subjects. This problem is ill-posed in the sense that the solution (if it exists)does not depend continuously on the data. A Fourier method is applied to formulate a regularized approximation solution, and some sharp error estimates are also given. 展开更多
关键词 反转热传导 病态问题 Fourier调整 抛物线方程 误差估计
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Estimation of Exhaust Gas Temperature of the Rocket Nozzle using Hybrid Approach 被引量:1
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作者 Manohar Karnal Beenish Batul 《Journal of Thermal Science》 SCIE EI CAS CSCD 2016年第6期485-491,共7页
In this paper the theoretical model is built for ZEpHyR(ZARM Experimental Hybrid Rocket) main engine which is being developed at ZARM institute,Bremen,Germany.The theoretical model is used to estimate the temperature ... In this paper the theoretical model is built for ZEpHyR(ZARM Experimental Hybrid Rocket) main engine which is being developed at ZARM institute,Bremen,Germany.The theoretical model is used to estimate the temperature of exhaust gas.The Conjugate Gradient Method(CGM) with Adjoint Problem for Function Estimation iterative technique is used to solve the Inverse Heat Conduction Problem(IHCP) to estimate the heat flux and internal wall temperature at the throat section of the nozzle.Bartz equation is used to calculate the convective heat transfer coefficient.The exhaust gas temperature is determined using the estimated heat flux,the wall temperature at internal surface of nozzle and the heat transfer coefficient.The accuracy of CGM iterative scheme to solve the IHCP is also investigated and its results are presented. 展开更多
关键词 Rocket iterative Conjugate exhaust convective nozzle throat deviation prior institute
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