[1] NOLL T E, ISHMAEL S D, HENWOOD B, et al. Technical findings, lessons learned, and recommendations resulting from the helios prototype vehicle mishap:NASA-20070022260[R]. Washington, D.C.:National Aeronautics and Space Admin Langley Research Center, 2007.
[2] WINDTE J, SCHOLZ U, RADESPIEL R. Validation of the RANS-simulations of laminar separation bubbles on airfoils[J]. Aerospace Science and Technology, 2006, 10(6):484-494.
[3] 刘沛清. 空气螺旋桨理论及其应用[M]. 北京:北京航空航天大学出版社, 2006:55-82. LIU P Q. Air propeller theory and application[M]. Beijing:Beihang University Press, 2006:55-82 (in Chinese).
[4] 段中喆, 刘沛清, 屈秋林. 修正的动力盘模型与三维模拟螺旋桨滑流比较[J].北京航空航天大学学报, 2013, 39(5):585-589. DUAN Z Z, LIU P Q, QU Q L. Slipstream characters comparison of improved actuator disk model and 3D propeller numerical simulation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(5):585-589 (in Chinese).
[5] 徐家宽, 白俊强, 黄江涛, 等. 考虑螺旋桨滑流影响的机翼气动优化设计[J]. 航空学报, 2014, 35(11):2910-2920. XU J K,BAI J Q,HUANG J T, et al. Aerodynamic optimization design of wing under the interaction of propeller slipstream[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(11):2910-2920 (in Chinese).
[6] NICOLAS T, CHRISTIAN B, NIKOLAUS A A. Numerical and experimental analysis of a generic fan-in-wing configuration[J]. Journal of Aircraft, 2009, 46(2):656-666.
[7] TSUNG L L, PAN K C. Application of the sliding mesh technique for helicopter rotor flow simulation[J]. Journal of Aeronautics, Astronautics and Aviation, 2012, 44(3):201-210.
[8] 王红波, 祝小平, 周洲, 等. 太阳能无人机螺旋桨滑流气动特性分析[J]. 西北工业大学学报, 2015, 33(6):913-920. WANG H B, ZHU X P, ZHOU Z, et al. Aerodyanmic investigation on propeller slipstream flows for solar powered airplanes[J]. Journal of Northwestern Polytechnical University, 2015, 33(6):913-920 (in Chinese).
[9] 徐华舫. 亚、超音速常位流的面元法[M]. 北京:国防工业出版社, 1981:159-190. XU H F. Panel methods of subsonic and supersonic flows[M]. Beijing:National Defense Industry Press, 1981:159-190 (in Chinese).
[10] KATZ J, PLOTKIN A. Low speed aerodynamics[M]. Cambridge:Cambridge University Press, 2000:207-217.
[11] WILLIS D J, JAIME P, JACOB K W. A combined pFFT-multipole tree code, unsteady panel method with vortex particle wakes[J]. International Journal for Numerical Methods in Fluids, 2007, 53(8):1399-1422.
[12] 李凤蔚.空气与气体动力学引论[M]. 西安:西北工业大学出版社, 2007:253-256. LI F W. Air and gas dynamic theory[M]. Xi'an:Northwestern Polytechnical University Press, 2007:253-256 (in Chinese).
[13] 魏鹏. 旋翼非定常流场的黏性涡数值模拟方法及其混合方法的研究[D]. 南京:南京航空航天大学, 2012:11-28. WEI P. Research on viscous vortex numerical algorithm and its hybrid method for rotor unsteady flowfield[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2012:11-28 (in Chinese).
[14] CHORIN A J. Numerical study of slightly viscous flow[J]. Journal of Fluid Mechanics, 1973, 57(4):785-796.
[15] HE C J, ZHAO J G. Modeling rotor wake dynamics with viscous vortex particle method[J]. AIAA Journal, 2009, 47(4):902-915.
[16] ELDREDGE J D, LEONARD A, COLONIUS T. A general deterministic treatment of derivatives in particle methods[J]. Journal of Computational Physics, 2002, 180(2):686-709.
[17] JOIN L H. Calculation of potential flow about arbitrary three dimensional lifting bodies:AD755840[R]. California:McDonnell Douglas Corporation, 1972.
[18] CALABRETTA J. A three dimensional vortex particle-panel code for modeling propeller-airframe interaction[D]. California:California Polytechnic State University, 2010:134-139.
[19] MCGHEE R J, WALKER B S, MILLARD B F. Experimental results for the eppler 387 airfoil at low Reynolds numbers in the langley low-turbulence pressure tunnel:NASA TM 4062[R]. Washington, D.C.:NASA Langley Research Center, 1988.
[20] CARADONNA F X, TUNG C. Experimental and analytical studies of a model helicopter rotor in hover:NASA TM-81232[R]. Washington, D.C.:NASA, 1981.
[21] BRAND A G, MCMAHON H M, KOMERATH N M. Surface pressure measurements on a body subject to vortex wake interaction[J]. AIAA Journal, 1989, 27(5):569-574.
[22] VELDHUIS L M. Propeller wing aerodynamic interference[D]. Delft:Delft University of Technology, 2005:187-191. |