Prediction of skin-friction and heat transfer from compressible turbulent boundary layers in rocket nozzles

Prediction of local skin-friction coeffi

Prediction of local skin-friction coefficient by transformation of the compressible boundary layer with heat transfer

✍ P.K. Chang; H.B. Nottage 📂 Article 📅 1961 🏛 Elsevier Science 🌐 English ⚖ 556 KB

This paper presents a transformation between compressible and incompressible two-dimensional and axisymmetric boundary-layer flows. The transformation may be used to predict local skin-friction coefficients for laminar and for turbulent flows, in zero as well as in favorable pressure gradient, and a