International Journal of Vehicle Structures and Systems

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Aerodynamics, Stability and Performance Characteristics of X-Tandem Aircrafts


Affiliations
1 Dept. of Aerospace Engg., SRM University, Chennai, India
 

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This paper details design, analysis and validation of tandem aircraft with one wing swept forward and the other wing swept backwards. The design objective is to investigate the aerodynamic and stability characteristics of this configuration created with the motive of exploiting the manoeuvring and post stall characteristics of a forward swept wing along with the structural robustness and reliable performance of the conventional aft-swept wing. Parameters such as wing sweep, wing position, anhedral and dihedral were varied to develop a range of designs. This gave considerable information regarding the aerodynamic and stability characteristics which enabled a preliminary design of a military combat aircraft exploiting this configuration. All performance characteristics and parameters of the final design compared with current operational military aircraft give a favourable picture regarding the effectiveness of this design.

Keywords

Aircraft Design, Combat Aircraft, Stability, Tandem Wing, Aerodynamics.
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  • W.P. Honderson and J.K. Huffman. 1975. Aero-dynamic characteristics of a tandem wing configuration at a mach number of 0.30, NASA Tech. Memorandum X-72779.

  • L.T. Nguyen, M.E. Ogburn, W.P. Gilbert, K.S. Kibler, P.W. Brown and P.L. Deal. 1979. Simulator study of stall/post-stall characteristics of a fighter airplane with relaxed longitudinal static stability, NASA Tech. Paper 1538.

  • T.M. Broering and Y. Lian. 2010. The effect of wing spacing on tandem wing aerodynamics, Proc. 28th AIAA Applied Aerodynamics Conf., Chicago, Illinois. https://doi.org/10.2514/6.2010-4385.

  • D.P. Raymer. 1992. Aircraft Design: A Conceptual Approach, 2nd Ed., AIAA Educational Series.

  • O. Gur, W.H. Mason and J.A. Schetz. 2010. Full configuration drag estimation, J. Aircraft, 47(4), 1356-1367. https://doi.org/10.2514/1.47557.

  • Kroo. 2005. Non-planar wing concepts for increased aircraft efficiency, VKI Lecture Series on Innovative Configurations and Advanced Concepts for Future Civil Aircraft, 1-29.

  • W.C. Moonan. 2010. Evaluation of the Aerodynamics of an Aircraft Fuselage Pod Using Analytical, CFD, and Flight Testing Techniques, Master Thesis, University of Tennesse, Knoxville.

  • E.J. Saltzman and J.W. Hicks. 1994. In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisons with contemporary aircraft), NASA Technical Paper 3414.


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  • Aerodynamics, Stability and Performance Characteristics of X-Tandem Aircrafts

Abstract Views: 621  |  PDF Views: 213

Authors

Ishaan Prakash
Dept. of Aerospace Engg., SRM University, Chennai, India
Prithwish Mukherjee
Dept. of Aerospace Engg., SRM University, Chennai, India

Abstract


This paper details design, analysis and validation of tandem aircraft with one wing swept forward and the other wing swept backwards. The design objective is to investigate the aerodynamic and stability characteristics of this configuration created with the motive of exploiting the manoeuvring and post stall characteristics of a forward swept wing along with the structural robustness and reliable performance of the conventional aft-swept wing. Parameters such as wing sweep, wing position, anhedral and dihedral were varied to develop a range of designs. This gave considerable information regarding the aerodynamic and stability characteristics which enabled a preliminary design of a military combat aircraft exploiting this configuration. All performance characteristics and parameters of the final design compared with current operational military aircraft give a favourable picture regarding the effectiveness of this design.

Keywords


Aircraft Design, Combat Aircraft, Stability, Tandem Wing, Aerodynamics.

References





DOI: https://doi.org/10.4273/ijvss.11.1.11