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2015 | 13 | 1 |
Tytuł artykułu

Numerical study on the standing morphology of an oblique detonation wave under the influence of an incoming boundary layer

Treść / Zawartość
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The influence of an incoming boundary layer to the standing morphology of an oblique detonation wave (ODW) induced by a compression ramp is numerically studied in this paper. The Spalart-Allmaras (SA) turbulence model is used to perform simulation of detonationboundary- layer interactions. Three different wall conditions are applied to realize control on the boundary-layer separation scales. Accordingly, different standing morphologies of the ODWs are obtained, including smooth ODW (without transverse wave) under no-slip, adiabatic wall condition with large-scale separation, abrupt ODW (with transverse wave) under no-slip, cold wall condition with moderate-scale separation, and bow-shaped detached ODW under slipwall condition without a boundary layer.
Wydawca

Czasopismo
Rocznik
Tom
13
Numer
1
Opis fizyczny
Daty
wydano
2015-01-01
otrzymano
2014-04-01
zaakceptowano
2014-07-28
online
2014-09-25
Twórcy
autor
  • Science and Technology on Scramjet Laboratory, National University of Defense Technology, College of Aerospace Science and Engineering, National University of Defense Technology, 410073 Changsha, China, zj706@vip.sina.com
autor
  • Science and Technology on Scramjet Laboratory, National University of Defense Technology, College of Aerospace Science and Engineering, National University of Defense Technology, 410073 Changsha, China, yuesefuliu@sina.com
autor
  • Science and Technology on Scramjet Laboratory, National University of Defense Technology, College of Aerospace Science and Engineering, National University of Defense Technology, 410073 Changsha, China
Bibliografia
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Typ dokumentu
Bibliografia
Identyfikatory
Identyfikator YADDA
bwmeta1.element.-psjd-doi-10_1515_phys-2015-0007
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