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Finite Wing Theory
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Author(s): Madhankumar G. (Sathyabama Institute of Science and Technology, India), Mothilal T. (KCG College of Technology, India), Kumar K. M. (St. Joseph's College of Engineering, India), Muralidharan G. (Surya Group of Institutions, India)and Mala D. (University College of Engineering, Panruti, India)
Copyright: 2022
Pages: 41
Source title:
Handbook of Research on Aspects and Applications of Incompressible and Compressible Aerodynamics
Source Author(s)/Editor(s): Sathish K. Kumar (Nehru Institute of Engineering and Technology, India)and Naren Shankar Radhakrishnan (Vel Tech Rangarajan Dr. Sagunthala R&D Institute of Science and Technology, India)
DOI: 10.4018/978-1-6684-4230-2.ch005
PurchaseView Finite Wing Theory on the publisher's website for pricing and purchasing information.
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Abstract
Wing design is a very complicated and intricate issue. It is not feasible to cover everything in this chapter; however, it is possible to discuss some of the essential ideas that underpin design for high lift and low drag. Lift may be increased in four ways for fixed air characteristics and free-stream speed: increased wing area, increased angle of attack, increased camber, increased circulation through the use of high-momentum fluid. One of the most important applications of potential flow theory was the study of lifting surfaces such as aircraft wings, since the boundary conditions on a complex geometry can significantly complicate any attempt to tackle the problem via analytical techniques, which involves some simplification assumptions in order to arrive at a solution. These assumptions will be related to the concept of three-dimensional thin wing issues in this chapter.
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