Preliminary Take-Off Analysis and Simulation of PrandtlPlane Commercial Aircraft

被引:0
作者
K. Abu Salem
G. Palaia
M. Bianchi
D. Zanetti
V. Cipolla
V. Binante
机构
[1] University of Pisa,Department of Civil and Industrial Engineering
[2] SkyBox Engineering S.r.l.,undefined
来源
Aerotecnica Missili & Spazio | 2020年 / 99卷 / 3期
关键词
PrandtlPlane; Box-Wing; Take-off; PARSIFAL;
D O I
10.1007/s42496-020-00056-0
中图分类号
学科分类号
摘要
The present paper deals with the take-off performance analysis of PrandtlPlane aircraft. The PrandtlPlane is a Box-Wing configuration based on Prandtl’s “Best Wing System” concept, which minimizes the induced drag once wingspan and lift are given. The take-off dynamics is simulated implementing the non-linear equations of motion in a numerical tool, which adopts a Vortex Lattice Method solver to evaluate the aerodynamics characteristics taking also ground effects into account. The take-off analysis is performed for both a PrandtlPlane and a reference monoplane, with the aim of comparing the performance of the two different architectures. The preliminary results show the potential advantages of the PrandtlPlane, such as runway length reduction and improved passenger comfort.
引用
收藏
页码:203 / 216
页数:13
相关论文
共 27 条
[1]  
Lee DS(2009)Aviation and global climate change in the 21st century Atmos. Environ. 43 3520-3537
[2]  
Schäfer WA(2019)Technological, economic, and environmental prospect of all-electric aircraft Nature Energy 4 160-166
[3]  
Cavallaro R(2016)Challenges, ideas, and innovations of joined-wing configurations: a concept from the past, an opportunity for the future Prog. Aerosp. Sci. undefined undefined-undefined
[4]  
Demasi L(2004)Design of the blended wing body subsonic transport J. Aircr. undefined undefined-undefined
[5]  
Liebeck RH(1987)Aerodynamic characteristics of biplanes with winglets J. Aircr. undefined undefined-undefined
[6]  
Gall PD(2016)Aerodynamic optimization trade study of a Box-Wing aircraft configuration J. Aircr. undefined undefined-undefined
[7]  
Smith HC(2014)Invariant formulation for the minimum induced drag conditions of nonplanar wing systems AIAA J. undefined undefined-undefined
[8]  
Gagnon H(2016)Central Reference Aircraft data System (CeRAS) for research community CEAS Aeronaut. J. undefined undefined-undefined
[9]  
Zingg DW(2019)Conceptual design of PrandtlPlane civil transport aircraft Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng. undefined undefined-undefined
[10]  
Demasi L(2018)PARSIFAL project: a breakthrough innovation in air transport Aerotecnica Missili Spazio undefined undefined-undefined