1 |
Zebbiche, T., "Stagnation Temperature Effect on the Prandtl Meyer Function", AIAA Journal, Vol. 45, No. 4, pp. 952-954, 2007
DOI
ScienceOn
|
2 |
Zebbiche, T. and Youbi, Z., "Supersonic Flow Parameters at High Temperature. Application for Air in Nozzles", The Aeronautical Journal, Vol., 111, 1115, Janvier 2007, pp. 31-40, 2007
DOI
|
3 |
Raltson, A. and Rabinowitz, A., "A First Course in Numerical Analysis", McGraw Hill Book Company, 1985
|
4 |
Zebbiche, T. and Youbi, Z., " Supersonic Two-Dimernsional Minimum Length Nozzle Design at High Temperature. Application for Air", AIAA Paper 2006-4599, July 2006
|
5 |
Zebbiche, T. and Youbi, Z., "Supersonic Plug Nozzle Design at High Temperature. Application for Air", 2006, AIAA Paper 2006-0592, Janvier 2006
|
6 |
Fletcher, C. A. J. " Computational Techniques for Fluid Dynamics: Specific Techniques for Different Flow Categories," Vol. II, Springer-Verlag, Berlin, 1988
|
7 |
Anderson, J. D. Jr., "Modern Compressible Flow: With Historical Perspective, Mc Graw-Hill Book Company, New York, 1982.
|
8 |
Stroud, A. H. and Secrest, D. H., "Gaussian Quadrature Formulas", Prentice-Hall, Inc., Engiewood Cliffs, N.J., 1966
|
9 |
Raltson, A., "A Family of Quadrature Formulas Which Achieve High Accurary in Composite Rules", J. Ass. Comput. Mach.", Vol. 6, pp. 384-394, 1959
DOI
|
10 |
Demidovtch B. et I. Maron I., "Elements de calcul numerique", 1987, Edition MIR, Moscou
|
11 |
Zebbiche, T., "Supersonic Axisymmetric Minimum Length Nozzle Conception at High Temperature", AIAA paper AIAA-2008-4110, 40th AIAA Thermophysics Conference, 23-26 June 2008, Washington, USA, 2008
|