赵攀峰,李大鹏,谭百贺,等.平流层飞艇热力学建模与仿真研究[J].合肥工业大学学报:自然科学版,2013,36(4): 501-505 Zhao Panfeng,Li Dapeng,Tan Baihe,et al.Themodynamic modeling and simulation of stratospheric airship[J].Journal of Hefei University of Technology:Natural Science,2013,36(4):501-505(in Chinese)
[2]
徐向华,程雪涛,梁新刚.平流层浮空器的热数值分析[J].清华大学学报:自然科学版,2009,49(11):1848-1851 Xu Xianghua,Cheng Xuetao,Liang Xingang.Thermalanalysis of a stratospheric airship[J].Journal of Tsinghua University:Science Technology,2009,49(11):1848-1851(in Chinese)
[3]
Stefan K.Thermaleffects on a high altitude air-ship[R].AIAA 1983-1984,1983
[4]
刘东旭,杨永强,吕明云,等.蒙皮材料热辐射特性对平流层浮空器氦气温度影响[J].北京航空航天大学学报,2010, 36(7):836-840 Liu Dongxu,Yang Yongqiang,Lü Mingyun,et al.Effect of envelope thermal radiative properties on the stratospheric superpressure LTA vehicle helium temperature[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(7):836-840(in Chinese)
[5]
黄迪,赵海涛,邱野,等.平流层飞艇蒙皮强度建模与仿真研究[J].计算机仿真,2013,30(1):150-153 Huang Di,Zhao Haitao,Qiu Ye,et al.Modeling and simulation analysis of stratospheric airship envelope[J].Computer Simulation,2013,30(1):150-153(in Chinese)
[6]
Komatsu K,Sano M,Kakuta Y.Development of high-specific-strength envelope materials[R].AIAA 2003-6765,2003
[7]
赵攀峰,李大鹏,谭百贺,等.平流层飞艇热力学建模与仿真研究[J].合肥工业大学学报:自然科学版,2013,36(4): 501-505 Zhao Panfeng,Li Dapeng,Tan Baihe,et al.Themodynamic modeling and simulation of stratospheric airship[J].Journal of Hefei University of Technology:Natural Science,2013,36(4):501-505(in Chinese)
[8]
徐向华,程雪涛,梁新刚.平流层浮空器的热数值分析[J].清华大学学报:自然科学版,2009,49(11):1848-1851 Xu Xianghua,Cheng Xuetao,Liang Xingang.Thermalanalysis of a stratospheric airship[J].Journal of Tsinghua University:Science Technology,2009,49(11):1848-1851(in Chinese)
[9]
刘东旭,杨永强,吕明云,等.蒙皮材料热辐射特性对平流层浮空器氦气温度影响[J].北京航空航天大学学报,2010, 36(7):836-840 Liu Dongxu,Yang Yongqiang,Lü Mingyun,et al.Effect of envelope thermal radiative properties on the stratospheric superpressure LTA vehicle helium temperature[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(7):836-840(in Chinese)
[10]
黄迪,赵海涛,邱野,等.平流层飞艇蒙皮强度建模与仿真研究[J].计算机仿真,2013,30(1):150-153 Huang Di,Zhao Haitao,Qiu Ye,et al.Modeling and simulation analysis of stratospheric airship envelope[J].Computer Simulation,2013,30(1):150-153(in Chinese)
[11]
杨世铭,陶文铨.传热学[M].北京:高等教育出版社,2006:263-274 Yang Shiming,Tao Wenquan.Heattransfer[M].Beijing:Higher Education Press,2006:263-274(in Chinese)
[12]
易洪雷,丁辛,陈守辉.PES/PVC膜材料拉伸性能的各向异性及破坏准则[J].复合材料学报,2005,22(6):98-102 Yi Honglei,Ding Xin,Chen Shouhui.Orthotropic behavior and strengh criterion of PES/PVC membrane materials under tensile loading[J].Acta Materiae Compositae Sinica,2005,22(6): 98-102(in Chinese)
[13]
杨世铭,陶文铨.传热学[M].北京:高等教育出版社,2006:263-274 Yang Shiming,Tao Wenquan.Heattransfer[M].Beijing:Higher Education Press,2006:263-274(in Chinese)
[14]
易洪雷,丁辛,陈守辉.PES/PVC膜材料拉伸性能的各向异性及破坏准则[J].复合材料学报,2005,22(6):98-102 Yi Honglei,Ding Xin,Chen Shouhui.Orthotropic behavior and strengh criterion of PES/PVC membrane materials under tensile loading[J].Acta Materiae Compositae Sinica,2005,22(6): 98-102(in Chinese)
[15]
李顺林.复合材料力学引论[M].上海:上海交通大学出版社,1986:63-64 Li Shunlin.Introduction to composite materical mechanics[M].Shanghai:Shanghai Jiao Tong University Press,1986:63-64(in Chinese)
[16]
李顺林.复合材料力学引论[M].上海:上海交通大学出版社,1986:63-64 Li Shunlin.Introduction to composite materical mechanics[M].Shanghai:Shanghai Jiao Tong University Press,1986:63-64(in Chinese)
[17]
Zhai H L,Euler A.Material challenges for lighter-than-air systems in high altitude applications[R].AIAA 2005-7488,2005
[18]
Cathey Jr H M,Fairbrother D A.The 2012 NASA ~532,200 m3 super pressure balloon test flight[R].AIAA 2013-1269,2013
[19]
Stefan K.Thermaleffects on a high altitude air-ship[R].AIAA 1983-1984,1983
[20]
Dubourg V,Daniel L.Operating a new French balloon system from a new Canadian launch site[R].AIAA 2013-1335,2013
[21]
Zhai H L,Euler A.Material challenges for lighter-than-air systems in high altitude applications[R].AIAA 2005-7488,2005
[22]
Komatsu K,Sano M,Kakuta Y.Development of high-specific-strength envelope materials[R].AIAA 2003-6765,2003