• Ujjal Kalita
• Pritam Saha

Abstract: Propeller is a mechanical device consist of hub and blades which produce thrust due to the rotational motion of blades mounted on the hub. In this study a low speed propeller driven private aircraft is designed which carries passenger with luggage and crew member. Geometric analysis is done for twisted wing configuration where two different airfoil NACA 23012 and NACA 23015 at tip of the wing and root of the wing are applied respectively. ANSYS is used for the creation of geometry and meshing and FLUENT is used as a solver to numerically analysis the airfoils of wing configuration. The performance parameters of the airplane is estimated as per the requirements.

Keywords: Airplane Design, Low speed airplane, NACA 23012, NACA 23015, Propeller driven Aircraft

"Conceptual Design and Performance Estimation of a 15-Seater Propeller Driven Private Airplane ", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.5, Issue 11, page no.447-453, November 2018, Available :http://www.jetir.org/papers/JETIRDS06071.pdf

"Conceptual Design and Performance Estimation of a 15-Seater Propeller Driven Private Airplane ", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.5, Issue 11, page no. pp447-453, November 2018, Available at : http://www.jetir.org/papers/JETIRDS06071.pdf