Experimental and Numerical Study on Wall Impedance Effects on Tollmien–Schlichting Waves-Reference-Cited by-同舟云学术

Experimental and Numerical Study on Wall Impedance Effects on Tollmien–Schlichting Waves

Published:2021-09-13 Issue: Volume: Page:1-12
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Rouviere Adrien¹,Méry Fabien¹^ORCID,Methel Jeanne¹,Vermeersch Olivier¹^ORCID,Forte Maxime¹

Affiliation:

1. ONERA—The French Aerospace Lab, F-31055 Toulouse, France

Funder

FP7 Joint Technology Initiatives Clean Sky 2, AIRFRAME Integrated Technology Demonstrator platform "AIRFRAME ITD"

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J060536

Reference20 articles.

1. van IngenJ. “A Suggested Semi-Empirical Method for the Calculation of the Boundary Layer Transition Region,” Delft Univ. of Technology (Technische Hogeschool Delft) Rept. VTH-74, Delft, The Netherlands, 1956, http://resolver.tudelft.nl/uuid:cff1 fb47-883f-4cdc-ad07-07d264f3fd10 [retrieved 2 Jan. 2019].

2. SmithA. M. O.GamberoniN. “Transition, Pressure Gradient and Stability Theory,” Douglas Aircraft Company Rept. ES 26388, El Segundo, CA, 31 Aug. 1956, https://engineering.purdue.edu/~aae519/BAM6QT-Mach-6-tunnel/otherpapers/smith-amo-eN-douglas-es26388-1956.pdf [retrieved 2 Jan. 2019].

3. Large-Scale Laminar Flow Tests Evaluated with Linear Stability Theory

4. An experimental study on the effects of two-dimensional positive surface defects on the laminar–turbulent transition of a sucked boundary layer

5. Transfer function method of measuring in‐duct acoustic properties. I. Theory

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