Role of CFD and Visualization Technique for Atmospheric Re-Entry Problems of H-II Orbiting Plane(HOPE)

• YAMAMOTO Yukimitsu

  National Aerospace Laboratory

Bibliographic Information

Other Title

• Role of CFD and Visualization Technique for Atomospheric Re-Entry Problems of H-2 Orbiting Plane(HOPE)
• Role of CFD and Visualization Technique

Abstract

Numerical Simulation is used for the aerodynamic design and flight analysis of re-entry spacecrafts, HOPE and HYFLEX. Several hundreds test runs are made to determine optimum configuration of HOPE. Real gas effects are also estimated by using non-equilibrium Navier-Stokes code and code validation are continued by comparing numerical results with conventional HWT, high enthalpy wind tunnel, and flight measurement data. CFD activity of enormously enlarged hypersonic flow simulations by Reentry spacecraft developments, enforces large scale parametric studies and parallel computations by NWT at NAL can correspond to these demands.

Journal

• Journal of the Visualization Society of Japan

  Journal of the Visualization Society of Japan 17 (Supplement1), 13-16, 1997

  The Visualization Society of Japan

Details

• CRID: 1390282679597131648
• NII Article ID: 10002674490
• NII Article ID: 130003648650
• NII Book ID: AN10374478
• DOI: 10.3154/jvs.17.supplement1_13
• ISSN: 1884037X
• ISSN: 09164731
• NDL BIB ID: 4247016
• Web Site: https://ndlsearch.ndl.go.jp/books/R000000004-I4247016
• Text Lang: en
• Data Source:
  • JaLC
  • NDL
  • Crossref
  • CiNii Articles
• Abstract License Flag: Disallowed