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

Masanori Hayashi; Shigeru Aso; Anzhong Tan

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

Masanori Hayashi, Shigeru Aso, Anzhong Tan

Space Systems Engineering

Research output: Contribution to journal › Article › peer-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 language	English
Pages (from-to)	231-239
Number of pages	9
Journal	Memoirs of the Kyushu University, Faculty of Engineering
Volume	47
Issue number	4
Publication status	Published - Dec 1 1987

All Science Journal Classification (ASJC) codes

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

Cite this

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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.",

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AU - Aso, Shigeru

AU - Tan, Anzhong

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N2 - 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.

AB - 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.

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

Abstract

All Science Journal Classification (ASJC) codes

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