Open Access
Issue
MATEC Web Conf.
Volume 316, 2020
2020 6th Asia Conference on Mechanical Engineering and Aerospace Engineering (MEAE 2020)
Article Number 04006
Number of page(s) 8
Section Aerospace Engineering
DOI https://doi.org/10.1051/matecconf/202031604006
Published online 01 July 2020
  1. Ou C., JI H. L, Xiao H.S., et al. Key problems in structure and thermal protection for MF-1 model testing flight vehicle [J]. Acta Aerodynamica sinica, 2017, 35(5):742-749. [Google Scholar]
  2. Yang Q T, Zhou Y, Yuan X X, et al. Surface pressure and temperature measurement technology in MF-1 modelling flight test[J]. Acta Aerodynamica sinica, 2017, 35(5):732-741. [Google Scholar]
  3. He Z C, CHE J, XIAO H S, et al. Trajectory design and Monte Carlo flight simulation for MF-1[J]. Acta Aerodynamica sinica, 2019, 37(2):201-206. [Google Scholar]
  4. Shehret Tilvaldyev, Erwin Martinez, Jorge FloresGaray, and Alfredo Villanueva Montellano, “Distribution of Dynamic Pressure in Micro-Scale of Subsonic Airflow around Symmetric Objects at Zero Angle of Attack, ” International Journal of Mechanical Engineering and Robotics Research, Vol. 6, No. 3, pp. 226-231, May 2017. DOI: 10.18178/ijmerr.6.3.226-231. [CrossRef] [Google Scholar]
  5. Yury I. Dimitrienko, Mikhail N. Koryakov, and Andrey A. Zakharov, “Computational Simulation of Conjugated Problem of External Aerodynamics and Internal Heat and Mass Transfer in High-Speed Aircraft Composite Construct, ” International Journal of Mechanical Engineering and Robotics Research, Vol. 6, No. 1, pp. 58-64, January 2017. DOI: 10.18178/ijmerr.6.1.58-64 [CrossRef] [Google Scholar]
  6. Kimmel, R. L. Aerothermal Design for the HIFiRE-1 flight Vehicle[C]. AIAA 2008-4034, June 2008. [Google Scholar]
  7. Adamczak, D., Alesi, H., Frost, M. HIFiRE-1: Payload Design, Manufacture, Ground Test, and Lessons Learned[C]. AIAA paper 2009-7294, October 2009. [Google Scholar]
  8. Roger L. Kimmel, David Adamczak. Hifire-1 Background and Lessons Learned[C]. AIAA paper 2012-1088, January 2012. [Google Scholar]
  9. Schneider, S. P. Flight Data for Boundary-Layer Transition at Hypersonic and Supersonic Speeds[J]. Journal of Spacecraft and Rockets, vol. 36, no. 1, January-February 1999. [CrossRef] [Google Scholar]
  10. Stetson, K. F. Nosetip Bluntntess Effects on Cone Frustum Boundary Layer Transition in Hypersonic Flow[C]. AIAA paper 83-1763, July 1983. [Google Scholar]
  11. Kimmel, R. L., Adamczak, D., Gaitonde, D., Rougeux, A., Hayes, J. R., HIFiRE-1 Boundary Layer Transition Experiment Design[C]. AIAA paper 2007-0534, January 2007. [Google Scholar]
  12. Johnson, H. B., Alba, C. R., Candler, G. V., MacLean, M., Wadhams, T, and Holden, M. Boundary Layer Stability Analysis of the Hypersonic International Flight Research Transition Experiments[C]. AIAA Journal of Spacecraft and Rockets, vol. 45, no. 2, March-April 2008. [CrossRef] [Google Scholar]
  13. Stainback, C. P. Effect of Unit Reynolds Number, NoseBluntness, Angle of Attack, and Roughness on Transition on a 5°Half -Angle Cone at Mach 8[C]. NASA TN D-4961, January 1969. [Google Scholar]
  14. Liu CHU-ping, Yang Qing-tao, et al. Heatflux measurement in aerothermodynamics and thermal protection tests [M]. Beijing: National Defense Industry Press, 2013. [Google Scholar]
  15. Zhang Shou-yan, Hui Yu-xin, et al. Modeling Free flight [M]. Beijing: National Defense Industry Press, 2002. [Google Scholar]

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