Summary
If a thin flat plate initially with an arbitrary temperature distribution along its length is suddenly moved from rest at a constant velocity through the air, the aerodynamic heating by boundary layer friction gradually changes the plate temperature to the adiabatic equilibrium value. The solution to this problem is obtained and illustrated by an example.
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Bibliography
Chapman, D., and Rubesin, M.: Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface Temperature, Journal of Aeronautical Sciences, Volume 16, No. 9, September, 1949, pp. 547–565.
Crocco, L.: Lo Strato Limite Laminare Nie Gas (The Laminar Boundary Layer in Gases). Monographie Scientifiche di Aeronautica, No. 3, December 1946, pp. 1–78.
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© 1955 Springer Fachmedien Wiesbaden
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Emmons, H.W. (1955). The non-steady aerodynamic heating of a plate. In: Görtler, H., Tollmien, W. (eds) 50 Jahre Grenzschichtforschung. Vieweg+Teubner Verlag, Wiesbaden. https://doi.org/10.1007/978-3-663-20219-6_36
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DOI: https://doi.org/10.1007/978-3-663-20219-6_36
Publisher Name: Vieweg+Teubner Verlag, Wiesbaden
Print ISBN: 978-3-663-19879-6
Online ISBN: 978-3-663-20219-6
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