Simulations and Models for Aspiration in a Supersonic Flow Using OVERFLOW-Reference-Cited by-同舟云学术

Simulations and Models for Aspiration in a Supersonic Flow Using OVERFLOW

Published:2015-07 Issue:7 Volume:53 Page:2052-2056
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Wukie Nathan A.¹,Orkwis Paul D.¹,Turner Mark G.¹,Duncan Sean¹

Affiliation:

1. Department of Aerospace Engineering, University of Cincinnati, Cincinnati, Ohio 45221

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053214

Reference20 articles.

1. LapsaA. P. “Experimental Study of Passive Ramps for Control of Shock-Boundary Layer Interactions,” Ph.D. Thesis, Univ. of Michigan, Ann Arbor, MI, 2009.

2. Multi-Row Micro-Ramp Actuators for Shock Wave Boundary-Layer Interaction Control

3. Flow coefficient behavior for boundary layer bleed holes and slots

4. Experimental investigation of the effect of a single bleed hole on a supersonic turbulent boundary-layer

5. Flow physics of a normal-hole bled supersonic turbulent boundary layer

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