Open Access Open Access  Restricted Access Subscription Access
Open Access Open Access Open Access  Restricted Access Restricted Access Subscription Access

Sizing of Wing and Wing Section for a Subsonic Jet Trainer Aircraft


Affiliations
1 Bhubaneswar Engineering College, Bhubaneswar, Odisha, India
     

   Subscribe/Renew Journal


This paper provides the procedure to calculate the sizing of wing, flap and airfoil selection. In this a subsonic jet trainer was taken for case study, for which above sizing were done. Initially symmetric and cambered airfoil were selected to find out suitable airfoil for this type of aircraft. Lift and drag coefficient were estimated for better performance to select the wing section. NACA three different series (Five digit, 1-series and 6-series) are taken for the calculation part. All the calculation were done for the velocity of 277.78 m/s (Reynold No of 8.45 x 106).

Keywords

Airfoil, NACA, Wing.
User
Subscription Login to verify subscription
Notifications
Font Size

  • “ Jane’s All the World’s Aircrafts”
  • www.Airliners.net
  • “Jane’s Engine Manual”
  • Flap Selection Manual
  • Theory of Wing Sections

Abstract Views: 10

PDF Views: 1




  • Sizing of Wing and Wing Section for a Subsonic Jet Trainer Aircraft

Abstract Views: 10  |  PDF Views: 1

Authors

S. K. Samal
Bhubaneswar Engineering College, Bhubaneswar, Odisha, India

Abstract


This paper provides the procedure to calculate the sizing of wing, flap and airfoil selection. In this a subsonic jet trainer was taken for case study, for which above sizing were done. Initially symmetric and cambered airfoil were selected to find out suitable airfoil for this type of aircraft. Lift and drag coefficient were estimated for better performance to select the wing section. NACA three different series (Five digit, 1-series and 6-series) are taken for the calculation part. All the calculation were done for the velocity of 277.78 m/s (Reynold No of 8.45 x 106).

Keywords


Airfoil, NACA, Wing.

References