Stagnation temperature effect on the Prandtl Meyer function

AIAA Journal

Volumn 45, Issue 4, 2007, Pages 952-954

  Zebbiche, Toufik ^a,b  

^a UNIVERSITY OF BLIDA   (Algeria)

^b Department of Aeronautics   (France)

Author keywords

[No Author keywords available]

Indexed keywords

PERFECT GAS (PG); POLYNOMIAL INTERPOLATION; PRANDTL MEYER (PM) FUNCTION;

INTEGRATION; INTERPOLATION; POLYNOMIALS; PRESSURE EFFECTS; PROBLEM SOLVING; SUPERSONIC FLOW; THERMAL EFFECTS;

PRANDTL NUMBER;

EID: 34247342118     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.24868     Document Type: Article

References (9)

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3. Zebbiche, T., and Youbi, Z., "Supersonic Two-Dimensional Minimum Length Nozzle Design at High Temperature. Application for Air," AIAA Paper 2006-4599, July 2006.
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7. Zebbiche, T., and Youbi, Z., "Fonction de Prandtl Meyer A Haute Température," Conférences Internationales sur la Mécanique Avancée, CIMA'04 [CD-ROM], University M'hamed Bougara, Boumerdès, Algérie, Dec. 2004.
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9. Fletcher, C. A. J., Computational Techniques for Fluid Dynamics: Specific Techniques for Different Flow Categories, Vol. 2, Springer-Verlag, Berlin, 1988.