Viscous Air flow Theory

A V Balakrishnan
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A V Balakrishnan: University of California, Department of Electrical Engineering Department of Mathematics

Chapter Chapter 7 in Aeroelasticity, 2012, pp 327-336 from Springer

Abstract: Abstract In this chapter we extend the theory allowing for nonzero viscosity. The field equations then are the Navier–Stokes equations, a subject in fluid dynamics of intense research activity, but still replete with many open problems. Our interest here is again on the effect of viscosity on the wing-structure response rather than the flow itself. The extant aeroelastic literature on this aspect is all computational 82, 83, 93].

Keywords: Field Equation; Stokes Equation; Mathematical Justification; Flexible Wing; Kutta Condition (search for similar items in EconPapers)
Date: 2012
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DOI: 10.1007/978-1-4614-3609-6_7

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