李 峰, 叶正寅, 高 超. 新型浮升一体化飞艇的总体性能和应用研究[J]. 工程力学, 2013, 30(3): 437-444, 458. DOI: 10.6052/j.issn.1000-4750.2011.10.0677
引用本文: 李 峰, 叶正寅, 高 超. 新型浮升一体化飞艇的总体性能和应用研究[J]. 工程力学, 2013, 30(3): 437-444, 458. DOI: 10.6052/j.issn.1000-4750.2011.10.0677
LI Feng, YE Zheng-yin, GAO Chao. OVERALL PERFORMANCE AND APPLICATION RESEARCH ON A NEW TYPE BUOYANCY-LIFTING AIRSHIP[J]. Engineering Mechanics, 2013, 30(3): 437-444, 458. DOI: 10.6052/j.issn.1000-4750.2011.10.0677
Citation: LI Feng, YE Zheng-yin, GAO Chao. OVERALL PERFORMANCE AND APPLICATION RESEARCH ON A NEW TYPE BUOYANCY-LIFTING AIRSHIP[J]. Engineering Mechanics, 2013, 30(3): 437-444, 458. DOI: 10.6052/j.issn.1000-4750.2011.10.0677

新型浮升一体化飞艇的总体性能和应用研究

OVERALL PERFORMANCE AND APPLICATION RESEARCH ON A NEW TYPE BUOYANCY-LIFTING AIRSHIP

  • 摘要: 开发具有高气动效率的浮升一体化飞艇对高空信息平台的发展具有重要的科学研究价值。基于NACA系列翼型的新型排翼式浮升一体化飞艇不仅具有相当可观的体积效率,而且还有较好的气动性能。为了综合考察排翼式浮升一体化飞艇的实用价值和经济收益,以更具有工程应用前景的平流层为设计平台,在一定的总设计载荷条件下,研究了排翼式布局的浮升特性,并对其总体性能和技术参数进行了详细的分析和评估。研究表明:在一定的速度范围内,排翼式浮升一体化飞艇具有优良的总体性能和实用价值。浮升一体化布局可以以更小的代价使飞艇的自重降低,有效载荷和单位生产率提高,因此在飞艇的的设计中不应一味追求阻力的最小化,而需要在低阻力与小尺寸之间进行权衡和折衷。

     

    Abstract: It has important scientific value to develop the buoyancy-lifting airship with higher aerodynamic efficiency. The new type tandem buoyancy-lifting airship, based on the NACA aerofoil, has considerable volume efficiency and aerodynamic efficiency. In order to examine the utility value and economy benefit at the design load condition,the buoyancy-lifting characteristics of tandem configuration in stratospheric platform are studied. Furthermore, its total performance and technical parameters are analyzed. Tandem buoyancy-lifting airship has excellent performance and utility value. As a result, its deadweight is decreased and payload and specific productivity are increased with smaller cost. Therefore, it is not advisable to overly pursue the minimization of drag. Contrarily, we need to seek a compromise between low drag and small dimension.

     

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