References
- Anderson J. D. Jr., 'Fundamentals of Aerodynamics.' McGraw-Hill Book Company. New York. 1988.
- Zucker R. D. and Bilbarz O.. 'Fundamentals of Gas Dynamics.' John Wiley & Sons, New Jersey. 2002.
-
Zebbiche T and Youbi Z.. 'Effect of Stagnation Temperature on Supersonic Flow Parameters. Application for Air in Nozzles.' The Aeronautical Journal. Vol. 111,
$N^{\circ}$ 1115. Jan. 2007. PP. 31-40. https://doi.org/10.1017/S0001924000001731 - Oosthuisen P. H. and Carscallen W. E., 'Compressible Fluid Flow,' McGraw Hill, New York, 1997.
- Ralston A. and Rabinowitz P., 'A First Course in Numerical Analysis', McGraw Hill Book Company, 1985.
- Zebbiche T. and Youbi Z., 'Super sonic Flow Parameters at High Temperature. Application for Air in Nozzles,' DGLR-20 05-256, Germany.
- Anderson J.. Jr., "Modern Compressible Flow: With Histori cal Perspective," McGraw Hill Book company, New York, 1982.
- Comolet R., "Mecanique Experimentale des Fluides. Statique et Dyna mique des Fluides Non Visqueux," Tome 1, 3eme Edition, Masson,1979.
- Dernidovitch B. and I. Maron., "Elements de calcul numerique," Editions Mir, Moscow, 1987.
- McLain D. H., "Drawing contours from arbitrary data points : The Computer Journal, Vol. 17, PP. 318-324, 1974 https://doi.org/10.1093/comjnl/17.4.318
- Powell M. J. D., "On the Maximum Error of Polynomial Approximation Defined by Interpolation and by Least Squares Criteria," Comput. J., Vol. 9, PP. 404-407, 1978. https://doi.org/10.1093/comjnl/9.4.404
- Zebbiche T. and Youbi Z., " Super sonic Two-Dimernsional Minimum Length Nozzle Design at High Temperature. Application for Air," AIAA-2006-4599, 42st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Sacramento, California, July 09-12,2006.
- 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.
- Hill. P. G. and Peterson C.R., Mechanics and Thermodynamics of Propulsion, Addition-Wesley Publishing Company Inc., New York, 1965.
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