• INFRARED
  • Vol. 43, Issue 1, 26 (2022)
Wei-bo SHI, Hai-hao SUN, Zhe-feng YU, An-hua SHI, and Yi-lei SHI*
Author Affiliations
  • [in Chinese]
  • show less
    DOI: 10.3969/j.issn.1672-8785.2022.01.005 Cite this Article
    SHI Wei-bo, SUN Hai-hao, YU Zhe-feng, SHI An-hua, SHI Yi-lei. The Analysis of Infrared Radiation Characteristics of HTV-2-like Hypersonic Gliding Vehicle Body[J]. INFRARED, 2022, 43(1): 26 Copy Citation Text show less
    References

    [1] Walker S H, Sherk J. The DARPA/AF Falcon Program: The Hypersonic Technology Vehicle # 2 (HTV-2) Flight Demonstration Phase[C]. Dayton:15th International Space Planes and Hypersonic Systems and Technologies Conference,2008.

    [4] Niu Q L, Yang S, He Z H, et al. Numerical study of infrared radiation characteristics of a boost-gliding aircraft with reaction control systems[J]. Infrared Physics & Technology, 2018, 92: 417-428.

    [6] Cooke J C. An Axially Symmetric Analogue for General Three-dimensional Boundary Layers[R]. British Ministry of Aviation: Aeronautical Research Council TR R&M 3200, 1961.

    [12] Engel C D, Praharaj S C. MINIVER upgrade for AVID system, VOL.I: LANMIN user′s manual, NASA CR-172212[R]. Washington D C: NASA, 1983.

    [14] Kemp N H, Riddell F R. Heat Transfer to Satellite Vehicles Reenters the Atmosphere[J]. Journal of Jet Propulsion, 1957, 27(2): 132-137.

    [15] Zoby E V, Moss J N, Sutton K. Approximate convective-heating equations for hypersonic flows[J]. Journal of Spacecraft and Rockets, 1981, 18(1): 64-70.

    [17] Marvin J G. CFD Validation Experiments for Hypersonic Flows[C]. Nashville: 17th Aerospace Ground Testing Conference, 1992.

    SHI Wei-bo, SUN Hai-hao, YU Zhe-feng, SHI An-hua, SHI Yi-lei. The Analysis of Infrared Radiation Characteristics of HTV-2-like Hypersonic Gliding Vehicle Body[J]. INFRARED, 2022, 43(1): 26
    Download Citation