Relation Between Geometry and Wake Characteristics of a Supersonic Microramp-Reference-Cited by-同舟云学术

Relation Between Geometry and Wake Characteristics of a Supersonic Microramp

Published:2021-11 Issue:11 Volume:59 Page:4501-4513
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Tambe Sumit¹^ORCID,Schrijer Ferry¹^ORCID,van Oudheusden Bas¹^ORCID

Affiliation:

1. Delft University of Technology, 2629HS Delft, The Netherlands

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J059868

Reference34 articles.

1. Micro-vortex generators for shock wave/boundary layer interactions

2. Shock wave/turbulent boundary layer interaction and its control

3. GiepmanR. “Flow Control for Oblique Shock Wave Reflections,” Ph.D. Dissertation, Delft Univ. of Technology, Delft, The Netherlands, 2016. 10.4233/uuid:597489bb-0b41-4da2-8ec4-b1bc390f8d2c

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4. Direct Numerical Simulation of Boundary Layers over Microramps: Mach Number Effects;AIAA Journal;2023-10-24

5. Flow Control Using MVG in Shock Wave/Boundary Layer Interaction;Lecture Notes in Mechanical Engineering;2022-09-25