UNSTEADY AERODYNAMIC HEATING PHENOMENA IN THE INTERACTION OF SHOCK WAVE/TURBULENT BOUNDARY LAYER.

Masanori Hayashi, Shigeru Aso, Anzhong Tan

Research output: Contribution to journalArticlepeer-review

2 Citations (Scopus)

Abstract

Fluctuations of heat transfer have been measured in the regions of interaction between oblique shock waves and turbulent boundary layers. A new type of heat transfer rate gauge with high spatial resolution and fast response was used for the measurements of heat transfer rates. Results are compared with the wall pressure fluctuation measurements done by authors at the same test conditions. Experiments were made at a nominal Mach number of 4.

Original languageEnglish
Pages (from-to)231-239
Number of pages9
JournalMemoirs of the Kyushu University, Faculty of Engineering
Volume47
Issue number4
Publication statusPublished - Dec 1 1987

All Science Journal Classification (ASJC) codes

  • Energy(all)
  • Atmospheric Science
  • Earth and Planetary Sciences(all)
  • Management of Technology and Innovation

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