A study of wing-fuselage interaction

✍ Scribed by M. A. Khan; T. Cebeci

• Publisher: Springer
• Year: 1986
• Tongue: English
• Weight: 693 KB
• Volume: 20
• Category: Article
• ISSN: 0022-0833
• DOI: 10.1007/bf00044611

✦ Synopsis

The problem addressed is that of the initial profile appropriate for the calculation of the boundary layer on the wing at a wing-body junction. The geometry considered is such that the fuselage boundary layer reaches the interaction region still attached and it is shown that when the wing has curvature the boundary-layer component of velocity normal to the wing is turned inviscidly through a right angle to provide a (in general) non-zero profile to initiate the wing calculation.