Turbulent boundary layers with large free-stream to wall temperature ratio
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Engineering
Link
http://link.springer.com/content/pdf/10.1007/BF00997313.pdf
Reference12 articles.
1. Back, L.H.: Acceleration and cooling effects in laminar boundary layers — subsonic, transonic and supersonic speeds. AIAAJ. 8 (1970) 794–802
2. Blottner, F.N.: Finite difference methods of solution of the boundary layer equation. AIAAJ. 8 (1970) 193–205
3. Pletcher, R.H.: On a finite difference solution for the constant property turbulent boundary layer. AIAAJ. 7 (1969) 305–311
4. Cebecci, T.; Smith, A.M.O.; Mosinskis, G.: Calculation of compressible adiabatic turbulent boundary layers. AIAAJ. 8 (1970) 1974–1982
5. Less, L.: Laminar heat transfer over blunt-nosed bodies at hypersonic speeds. Jet Propulsion 26 (1956) 259–269
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1. Comment on "Dynamic Condensation";AIAA Journal;1985-11
2. Comment on "Laminar Stagnation-Point Heat Transfer for a Two-Temperature Argon Plasma";AIAA Journal;1985-11
3. Reply by Authors to J.A. Brandon;AIAA Journal;1985-11
4. Reply by Authors to H. Chuang;AIAA Journal;1985-11
5. Einflu\ der TemperaturabhÄngigkeit der Stoffwerte auf den WÄrmeübergang an der laminar überströmten ebenen Platte;Wärme- und Stoffübertragung;1982-09
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