Computational Flowfield Analysis of a Planetary Entry Vehicle
作者： Antonio Viviani , Giuseppe Pezzella
DOI: 10.5772/13504
关键词:
摘要: … take place in the flowfield past the hypersonic vehicle to assess its … non-equilibrium flowfield computations with a full reaction … occurs if the thermal shield is built with a noncatalytic TPM. …
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John David Anderson, Hypersonic and high temperature gas dynamics ,(2013)
John David Anderson, Computational fluid dynamics : the basics with applications McGraw-Hill. ,(1995)
Peter A. Gnoffo, Judy L. Shinn, Roop N. Gupta, Conservation equations and physical models for hypersonic air flows in thermal and chemical nonequilibrium NASA TP-2867. ,(1989)
Chul Park, Seokkwan Yoon, Calculation of real-gas effects on blunt-body trim angles AIAA Journal. ,vol. 30, pp. 999- 1007 ,(1989) , 10.2514/3.11020
Basil Hassan, Graham V. Candler, David R. Olynick, Thermo-chemical nonequilibrium effects on the aerothermodynamics of aerobraking vehicles Journal of Spacecraft and Rockets. ,vol. 30, pp. 647- 655 ,(1993) , 10.2514/3.26369
LESTER LEES, Laminar Heat Transfer Over Blunt-Nosed Bodies at Hypersonic Flight Speeds Journal of Jet Propulsion. ,vol. 26, pp. 259- 269 ,(1956) , 10.2514/8.6977
Peter A. Gnoffo, K. James Weilmuenster, H. Harris Hamilton, David R. Olynick, Ethiraj Venkatapathy, Computational Aerothermodynamic Design Issues for Hypersonic Vehicles Journal of Spacecraft and Rockets. ,vol. 36, pp. 21- 43 ,(1999) , 10.2514/2.3430
Antonio Viviani, Giuseppe Pezzella, Computational Flowfield Analysis over a Blunt-Body Reentry Vehicle Journal of Spacecraft and Rockets. ,vol. 47, pp. 258- 270 ,(2010) , 10.2514/1.40876
CHUL PARK, SEUNG-HO LEE, Validation of multi-temperature nozzle flow code NOZNT AIAA, 28th Thermophysics Conference. ,(1993) , 10.2514/6.1993-2862
David Olynick, Trajectory-Based Thermal Protection System Sizing for an X-33 Winged Vehicle Concept Journal of Spacecraft and Rockets. ,vol. 35, pp. 249- 257 ,(1998) , 10.2514/2.3338