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SCIENCE CHINA Physics, Mechanics & Astronomy, Volume 61, Issue 2: 024722(2018) https://doi.org/10.1007/s11433-017-9117-8

Hypersonic I-shaped aerodynamic configurations

Kai Cui1,2,*, Yao Xiao1,2, YingZhou Xu1,2, GuangLi Li1,2,*
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  • ReceivedAug 30, 2017
  • AcceptedOct 11, 2017
  • PublishedDec 18, 2017

Abstract

There is no abstract available for this article.


Funded by

National Natural Science Foundation of China(11372324)

Institute of Mechanics

Chinese Academy of Sciences(LHD2017TC01)

and the State Key Laboratory of High Temperature Gas Dynamics


Acknowledgment

This work was supported by the National Natural Science Foundation of China (Grant Nos. 11372324, and 11572333), and the State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences (Grant Nos. LHD2017TC01, LHD2017MS04, and LHD2017QN03).


References

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  • Figure 1

    Configuration and aerodynamic performance comparison between the HIAC and the reference model. (a) HIAC; (b) Ref; (c) Ma=5; (d) Ma=6; (e) Ma=7.

  • Table 1   Freestream conditions of numerical simulations

    Ma

    P0 (Pa)

    T0 (K)

    P (Pa)

    T (K)

    Re (m−1)

    5

    1.0×106

    345

    1.89×103

    58

    2.299×107

    6

    2.5×106

    465

    1.58×103

    57

    2.365×107

    7

    4.0×106

    590

    9.66×102

    55

    1.791×107

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