Investigation on Aerodynamic Analysis of Aircraft Boeing - 747
[1]
Saravana Kumar Sellappan, Department of Automobile Engineering, PSG College of Technology, Tamilnadu, India.
[2]
Niresh Jayarajan, Department of Automobile Engineering, PSG College of Technology, Tamilnadu, India.
[3]
Vijayakrishna Kanagarasu, Department of Mechanical Industrial Manufacturing Engineering, University of Toledo, Ohio, USA.
Aerodynamics simulation of an aircraft in real time may create financial impact and the time consumptions. Performing aerodynamic analysis using software tools may reduce the above said impacts in nature. In our work, a civilian aircraft model called Boeing 747-400 has been considered for study. Aircraft is modeled using Solid works 2014 with necessary boundary conditions and the same is analyzed using Ansys 14.5. Study describes the complete model structure generation and the aerodynamic analysis includes the preprocessor, modeling, mesh generation and the post processor of the Boeing 747 model.
Aerodynamics, Aircraft, Ansys, Boeing-747, Simulation, Solidworks
[1]
Shivasharanayya Hiremath, Anandkumar. S. Malipatil, “CFD Simulations of Aircraft Body with Different Angle of Attack and Velocity”, International Journal of Innovative Research in Science, Engineering and Technology, Vol. 3, Issue 10, October 2014, ISSN: 2319-8753.
[2]
Adam Kosík, “The CFD Simulation Of The Flow Around The Aircraft Using Open foam And Ansa”, 5th ANSA &μETA International Conference.
[3]
R. C. Gunness, jr., C. J. Knight, and E. D'sylud, ”Flow field analysis of aircraft G. P configurations using a numerical 'p solution to the three-dimensional”, small-disturbance equations unified supersonic/hypersonic, national aeronautics and space administration washington, d. C. February 1972.
[4]
HAM Peiris, PVS Nirmal, HMHHS Bandara, DM Mahindarathne, “Aerodynamics Analysis of F-16 Aircraft”, Proceedings of 8th International Research Conference, KDU, Published November 2015.
[5]
Bai-gang Mi, Hao Zhan, Bai-bing Chen, New Systematic CFD Methods to Calculate Static and Single Dynamic Stability Derivatives of Aircraft, Mathematical Problems in Engineering, Volume 2017 (2017), Article ID 4217217, 11 pages.
[6]
Manish Sharma, T. RatnaReddy, Ch. Indira Priyadarsini,“Flow Analysis over anF-16 Aircraft using Computational Fluid Dynamics”, International Journal of Emerging Technology and Advanced Engineering, ISSN 2250-2459, ISO 9001:2008 Certified Journal, Volume 3, Issue 5, May 2013.
[7]
Antony Jameson, McDonnell, Computational Aerodynamics for Aircraft Design, Reprinted from Science, Volume 245, pp. 361-371, 1989.
[8]
Adam Dziubiński, Piotr Jaśkowski, Tomasz Seredyn, CFD Analysis of Agricultural Aircraft Aerodynamic Characteristics, transactions of the institute of aviation, no. 4 (245), pp. 321-337, Warsaw 2016.
[9]
Statistical Data for the Boeing-747-400 Aircraft in Commercial Operations, Office of Aviation Research, Washington, D. C. 20591
[10]
Green, B. and Findlay, D., “CFD Analysis of the F/A-18E Super Hornet during Aircraft-Carrier Landing High-Lift Aerodynamic Conditions,” AIAA-2016-1768, SciTech 2016, San Diego, CA, Jan 2016.