60
M. Saleem et al.
Fig. 10 Pressure contour over the wing
From the flow analysis velocity and pressure contour has been found. From the
velocity contour, we have seen that the flow travelling through the surface of the
wing is smooth and streamline. C l /C d value has also been calculated from the flow
analysis as 19 at 5° angle of attack.
References
1. Baughn TV, Packman PF (1986) Finite element analysis of an ultralight aircraft. J Aircr 23(1):82–
86
2. Kesavulu A, AnandRaju F, Deva Kumar MLS (2014) Properties of aluminium fly ash metal
matrix composite. 3(11). ISSN: 2319-8753
3. Pawara PB, Utpat AA (2014) Analysis of composite material aircraft wing under static loading
condition. Elsevier
4. Rajappan R, Pugazhenthi V (2013) Finite element analysis of aircraft wing using composite
structure. IJES 2(2)
5. Mayurkymarkevadiya (2013) CFD Analysis of pressure coefficient for NACA 4412
6. Anderson JD Jr (2007) Introduction to flight, 5th edn. The McGraw-Hill Companies
7. Roskam J, Chuan-Tau (1997) Airplane aerodynamics and performance
8. Murugesan P, Thirumurugan P, Analytical and numerical investication of critical buckling
analysis of composite wing. Int J Modern Eng Res (IJMER)
9. Jones RT (2013) The spanwise distribution of lift for minimum induced drag of wings having
a given lift and a given bending moment. Int J Innov Res Sci Eng Technol 2(6). Tech. Rep.
TN-2249, NASA, Dec 1950
M. Saleem et al.
Fig. 10 Pressure contour over the wing
From the flow analysis velocity and pressure contour has been found. From the
velocity contour, we have seen that the flow travelling through the surface of the
wing is smooth and streamline. C l /C d value has also been calculated from the flow
analysis as 19 at 5° angle of attack.
References
1. Baughn TV, Packman PF (1986) Finite element analysis of an ultralight aircraft. J Aircr 23(1):82–
86
2. Kesavulu A, AnandRaju F, Deva Kumar MLS (2014) Properties of aluminium fly ash metal
matrix composite. 3(11). ISSN: 2319-8753
3. Pawara PB, Utpat AA (2014) Analysis of composite material aircraft wing under static loading
condition. Elsevier
4. Rajappan R, Pugazhenthi V (2013) Finite element analysis of aircraft wing using composite
structure. IJES 2(2)
5. Mayurkymarkevadiya (2013) CFD Analysis of pressure coefficient for NACA 4412
6. Anderson JD Jr (2007) Introduction to flight, 5th edn. The McGraw-Hill Companies
7. Roskam J, Chuan-Tau (1997) Airplane aerodynamics and performance
8. Murugesan P, Thirumurugan P, Analytical and numerical investication of critical buckling
analysis of composite wing. Int J Modern Eng Res (IJMER)
9. Jones RT (2013) The spanwise distribution of lift for minimum induced drag of wings having
a given lift and a given bending moment. Int J Innov Res Sci Eng Technol 2(6). Tech. Rep.
TN-2249, NASA, Dec 1950