1 |
Dernidovitch B. and I. Maron., "Elements de calcul numerique," Editions Mir, Moscow, 1987.
|
2 |
McLain D. H., "Drawing contours from arbitrary data points : The Computer Journal, Vol. 17, PP. 318-324, 1974
DOI
ScienceOn
|
3 |
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.
DOI
|
4 |
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.
|
5 |
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.
|
6 |
Hill. P. G. and Peterson C.R., Mechanics and Thermodynamics of Propulsion, Addition-Wesley Publishing Company Inc., New York, 1965.
|
7 |
Anderson J.. Jr., "Modern Compressible Flow: With Histori cal Perspective," McGraw Hill Book company, New York, 1982.
|
8 |
Comolet R., "Mecanique Experimentale des Fluides. Statique et Dyna mique des Fluides Non Visqueux," Tome 1, 3eme Edition, Masson,1979.
|
9 |
Anderson J. D. Jr., 'Fundamentals of Aerodynamics.' McGraw-Hill Book Company. New York. 1988.
|
10 |
Zucker R. D. and Bilbarz O.. 'Fundamentals of Gas Dynamics.' John Wiley & Sons, New Jersey. 2002.
|
11 |
Zebbiche T and Youbi Z.. 'Effect of Stagnation Temperature on Supersonic Flow Parameters. Application for Air in Nozzles.' The Aeronautical Journal. Vol. 111, 1115. Jan. 2007. PP. 31-40.
DOI
|
12 |
Oosthuisen P. H. and Carscallen W. E., 'Compressible Fluid Flow,' McGraw Hill, New York, 1997.
|
13 |
Ralston A. and Rabinowitz P., 'A First Course in Numerical Analysis', McGraw Hill Book Company, 1985.
|
14 |
Zebbiche T. and Youbi Z., 'Super sonic Flow Parameters at High Temperature. Application for Air in Nozzles,' DGLR-20 05-256, Germany.
|