Skip to main content
Disciplines
Automotive Business IT + Informatics Construction + Real Estate Electrical Engineering + Electronics Energy + Sustainability Insurance + Risk Finance + Banking Management + Leadership Marketing + Sales Mechanical Engineering + Materials
Events
DE
EN
Books
Journals
Topic Page
Marketing
Start single access now
Access for companies
EXTENDED SEARCH
Log in
Top
Published in:
Studies of Shock Wave Reflections and Interactions (Paul Vieille Lecture) Read chapter Read first chapter

2017 | OriginalPaper | Chapter

Role of Wall Temperature on Shock Train in a Rectangular Isolator

Authors : Lianjie Yue, Hongbo Lu, Yabin Xiao, Lihong Chen, Xinyu Chang

Published in: 30th International Symposium on Shock Waves 1

Publisher: Springer International Publishing

Log in

Activate our intelligent search to find suitable subject content or patents.

search-config
loading …

Abstract

Aimed at the problem of isolator being seriously heated by aeroheating, effects of wall temperature on flow characteristics of isolator are experimentally and numerically investigated. The results show that shock train is affected by the dual mechanism of isolator wall temperature and airflow total temperature. With an increase of wall temperature and a reduction of total temperature, the length of shock train increases. This tendency can be characterized by the variation of shock train length with ratio of wall temperature to total temperature. Based on numerical data, both the ratio of wall temperature to total temperature and specific heat ratio are introduced to modify the correlation of Waltrup and Billig for predicting shock train length of practical design with the coverage of more physical influencing factors.

Dont have a licence yet? Then find out more about our products and how to get one now:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

inform now

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

inform now

Springer Professional "Wirtschaft"

Online-Abonnement

Mit Springer Professional "Wirtschaft" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 340 Zeitschriften

aus folgenden Fachgebieten:

  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Versicherung + Risiko




Jetzt Wissensvorsprung sichern!

inform now
previous chapter Stabilization of Detonation Combustion of a Supersonic Flow due to Using the Special Form Plane Channel
next chapter The Correlation Between Detonation Cell Size and Ignition Delay Time
Literature
1.
Heiser, W.H., Pratt, D.T.: Hypersonic airbreathing propulsion. AIAA, Washington DC (1993)
2.
Curran, E.T., Murthy, S.N.B.: Scramjet propulsion. AIAA, Washington, DC (2001)
3.
Billig, F.S., Dugger, G.L., Waltrup, P.J. Inlet combustor interface problems in scramjet engines. The First International Symposium on Air Breathing Propulsion, Marseille, France, June 1972
4.
Mtsuo, K., Miyazato, Y., Kim, H.D.: Shock train and pseudo-shock phenomena in internal gas flows. Prog. Aerospace Sci. 35, 33–100 (1999)CrossRef
5.
Waltrup, P.J., Billig, F.S.: Structure of shock waves in cylindrical ducts. AIAA J 11(10), 1404–1408 (1973)CrossRef
6.
Carroll, B.F., Dutton, J.C.: Characteristics of multiple shock-wave/turbulent boundary-layer interactions in rectangular ducts. Jet Propul. 6(2), 186–193 (1990)CrossRef
7.
Carroll, B.E., Dutton, J.C.: Turbulence phenomena in a multiple normal shock Wave/turbulent boundary layer interaction. AIAA J. 30(1), 43–48 (1992)CrossRef
8.
Matsuo, K.: Shock train and pseudo-shock phenomena in supersonic internal flows. J. Thermal Sci. 12(3), 204–208 (2003)CrossRef
9.
Weiss, A., Grzona, A., Olivier, H.: Behavior of shock trains in a diverging duct. Exp. Fluids 49, 355–365 (2010)CrossRef
10.
Cuffel, R.F., Backf, L.H.: Flow and heat transfer measurements in a pseudo-shock region with surface cooling. AIAA J. 14(12), 1716–1722 (1976)CrossRef
11.
Fischer, C., Olivier, H. Experimental investigation of the internal flow field of a scramjet engine. AIAA pp. 2009–7369 (2009)
12.
Fischer, C., Olivier, H. Experimental investigation of the shock train in an isolator of a scramjet inlet. AIAA pp. 2011–2220 (2011)
13.
Lin, K.C., Tam, C.J., Jackson, K.R., et al. Characterization of shock train structures inside constant-area isolators of model scramjet combustors. AIAA pp. 2006–0816 (2006)
14.
Lin, K.C., Tam, C.J., Eklund, D.R., et al. Effects of temperature and head transfer on shock train structures inside constant-area isolators. AIAA pp. 2006–0817 (2006)
15.
Fischer, C., Olivier, H.: Experimental investigation of wall and total temperature influence on a shock train. AIAA J. 52(4), 757–766 (2014)CrossRef
Metadata
Title
Role of Wall Temperature on Shock Train in a Rectangular Isolator
Authors
Lianjie Yue
Hongbo Lu
Yabin Xiao
Lihong Chen
Xinyu Chang
Copyright Year
2017
Book
30th International Symposium on Shock Waves 1

Print ISBN: 978-3-319-46211-0

Electronic ISBN: 978-3-319-46213-4

Copyright Year: 2017

DOI
https://doi.org/10.1007/978-3-319-46213-4_72

Premium Partners

    Image Credits