Separation Length Scaling in Hypervelocity Double Cone Air Flows

  • A. B. Swantek
  • J. M. Austin
Conference paper

Introduction

A hallmark problem in the study of shockwave/boundary-layer interactions (SBLI) is the flow over a double cone. The system of conical shocks interact with a developing boundary layer to produce a region of flow separation. Due to the presence of real gas effects (defined here to mean any deviations from perfect gas behavior resulting from thermal transitions and chemical reactions), air simulations routinely fail to match experimental data at flow enthalpies greater than 6 MJ/kg [1]. The double cone flow has been identified as an exceptionally suitable model problem due to the sensitivity of the separation zone size and heat transfer rates to real gas effects [2]. Numerous researchers have investigated these flow fields both experimentally and computationally [3, 4, 5, 6, 7]. Many studies focus on the pressure and heat transfer distributions, in an effort to verify chemical and thermal models. The development of the shock system and separation zone has been investigated with varying configurations for both double cones [8] and double wedges [9].

Keywords

Mach Number Separation Zone Double Cone AIAA Aerospace Shock System 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Springer-Verlag Berlin Heidelberg 2012

Authors and Affiliations

  • A. B. Swantek
    • 1
  • J. M. Austin
    • 1
  1. 1.Dept. of Aerospace EngineeringUniversity of IllinoisUrbanaUSA

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