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

Masanori Hayashi, Shigeru Aso, Anzhong Tan

Research output: Contribution to journalArticle

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

Fingerprint

Aerodynamic heating
turbulent boundary layer
shock wave
Shock waves
aerodynamics
heat transfer
Boundary layers
Heat transfer
heating
Mach number
Gages
gauge
spatial resolution
Heating
Interaction
Aerodynamics
experiment
Experiments
rate
Fluctuations

All Science Journal Classification (ASJC) codes

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

Cite this

UNSTEADY AERODYNAMIC HEATING PHENOMENA IN THE INTERACTION OF SHOCK WAVE/TURBULENT BOUNDARY LAYER. / Hayashi, Masanori; Aso, Shigeru; Tan, Anzhong.

In: Memoirs of the Kyushu University, Faculty of Engineering, Vol. 47, No. 4, 01.12.1987, p. 231-239.

Research output: Contribution to journalArticle

@article{127a58e6f8dd47eb9b61ef514f465ac6,
title = "UNSTEADY AERODYNAMIC HEATING PHENOMENA IN THE INTERACTION OF SHOCK WAVE/TURBULENT BOUNDARY LAYER.",
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.",
author = "Masanori Hayashi and Shigeru Aso and Anzhong Tan",
year = "1987",
month = "12",
day = "1",
language = "English",
volume = "47",
pages = "231--239",
journal = "Memoirs of the Faculty of Engineering, Kyushu University",
issn = "1345-868X",
publisher = "Kyushu University, Faculty of Science",
number = "4",

}

TY - JOUR

T1 - UNSTEADY AERODYNAMIC HEATING PHENOMENA IN THE INTERACTION OF SHOCK WAVE/TURBULENT BOUNDARY LAYER.

AU - Hayashi, Masanori

AU - Aso, Shigeru

AU - Tan, Anzhong

PY - 1987/12/1

Y1 - 1987/12/1

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.

UR - http://www.scopus.com/inward/record.url?scp=0023566226&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=0023566226&partnerID=8YFLogxK

M3 - Article

AN - SCOPUS:0023566226

VL - 47

SP - 231

EP - 239

JO - Memoirs of the Faculty of Engineering, Kyushu University

JF - Memoirs of the Faculty of Engineering, Kyushu University

SN - 1345-868X

IS - 4

ER -