专利:
1.进出口形状可定制的内乘波式高超声速进气道及设计方法，中国发明专利，200810155271.9，2010
2.基于任意激波形状的内乘波式高超声速进气道及设计方法，中国发明专利，200810155897.X, 2010
3.进出口形状可定制的内乘波式高超声速进气道，中国实用新型专利，200820160752.4, 2009
4.基于任意激波形状的内乘波式高超声速进气道，中国实用新型专利，200820159849.3, 2009
论文:
1.Yancheng You, Heinrich Luedeke, Klaus Hannemann, Injection and Mixing in a Scramjet Combustor: DES and RANS Studies, Proceedings of the Combustion Institute, Online publication first,http://dx.doi.org/10.1016/j.proci.2012.10.001，2012. (SCI ，JCR2区)
2.Yancheng You, Heinrich Luedeke, Klaus Hannemann, On the flow physics of a low momentum flux ratio jet in a supersonic turbulent crossflow, Europhysics Letters, Vol.97,No. 2, 24001, 2012. (SCI ，JCR2区)
3.Yancheng You, Dewang Liang, Design concept of three-dimensional section controllable internal waverder hypersonic inlet, Science in China, 2009, v52(7): 2017-2028. (SCI, JCR4 区)
4.Yancheng You, Heinrich Luedeke, Volker Hannemann, Evaluation of turbulence models in predicting hypersonic and subsonic base flows using grid adaptation techniques, Chinese Journal of Aeronautics, 2012, Vol. 25 (3): 325-334. (SCI, JCR4 区)
5.Yancheng You, Dewang Liang, A non-linear eddy-viscosity view of shock wave/boundary layer interaction flow simulation, Shock Waves, In: Special Issue of 28th International Symposium on Shock Waves, pp. 465-470, ISBN 9783642256875, 2012.
6.Yancheng You, Heinrich Luedeke, Klaus Hannemann, Thino Eggers, Application of the Gamma-Re_theta_t Transition Model in High Speed Flows, AIAA 2012-5972, 2012.
7.Yancheng You, Klaus Hannemann, Numerical study of compressible mixing layers in HYSHOT II supersonic combustor, In: Proceeding of 7th European Symposium on Aerothermodynamics for Space Vehicles, ISBN: 9789292212568, 2011.
8.Yancheng You, Kai Osswald, Heinerich Luedeke, Volker Hannemann, Detached eddy simulation of the subsonic base flow with a side support, In: Progress in Hybrid RANS-LES Modelling, pp. 427-438, ISBN: 9783642318177, 2011.
9.Yancheng You, Dewang Liang, Guoping Huang, Cross section controllable hypersonic inlet design using streamline tracing and osculating axisymmetric concepts, AIAA-2007-5379, 2007, EI 收录号：20075010968232.
10.Yancheng You, Dewang Liang, Ke Cai, Numerical research of three-dimensional sections controllable internal waverider hypersonic inlet, AIAA-2009-0031, 2009, EI 收录号：20103813247062.
11.Yancheng You, Dewang Liang, Rongwei Guo. High enthalpy wind tunnel tests of three-dimensional section controllable internal waverider hypersonic inlet, AIAA-2009-0031, 2009, EI 收录号：20104813418977.
12.Yancheng You, Chengxiang Zhu, Dual waverider concept for the integration of hypersonic inward turning inlet and airframe forebody, AIAA-2009-7421, 2009, EI 收录号：20104413337200.
13.Yancheng You, An overview of the advantages and concerns of hypersonic inward turning Inlets, AIAA-2011-2269, 2011.
14.Yancheng You, Heinrich Luedeke, Klaus Hannemann, RANS and DES mixing layers investigations with the DLR TAU code, ESA deliverable report: D6.1.2-ACP7-GA-2008-211485, 2011.
15.Yancheng You, Heinerich Luedeke, Numerical investigation of a generic rocket base flows under subsonic conditions, Sonderforschungsbereich Transregio 40 - Jahresbericht Deutsche Forschungsgemeinschaft (DFG, German Science Foundation Report), 2011.
16.尤延铖, 梁德旺, 基于内乘波概念的三维变截面高超声速进气道, 中国科学E 辑:技术科学, 2009, v39(8): 1483-1494, EI 收录号：20092812186679.
17.尤延铖, 梁德旺, 对二维分离流涡黏性系数非线性分布的新认识, 力学学报, 2009, v41(2):145-154, EI 收录号：20091512029352.
18.尤延铖, 梁德旺, 黄国平, 内乘波式进气道内收缩基本流场研究, 空气动力学学报, 2009, v26(2):203-207, EI 收录号：20083111424455.
19.尤延铖, 梁德旺, 黄国平, 一种新型内乘波式进气道初步研究, 推进技术, 2006, v27(3):252-256, EI 收录号：20063510092444.
20.尤延铖，梁德旺，黄国平，郭荣伟, 高超声速三维内收缩式进气道/乘波前体一体化设计研究评述, 力学进展, 2009, v39(5):513-525.
