Numerical simulation of turbulent boundary layers with foreign gas transpiration using OpenFOAM-Reference-Cited by-同舟云学术

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Numerical simulation of turbulent boundary layers with foreign gas transpiration using OpenFOAM

Published:2019-05 Issue: Volume:158 Page:253-263
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Prokein Daniel,von Wolfersdorf Jens

Funder

University of Stuttgart

Helmholtz Alliance

Helmholtz Young Investigator’s Group

High Temperature Management in Hypersonic Flight

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference42 articles.

1. Comparison of Effectiveness of Convection-, Transpiration-, and Film-Cooling Methods with Air as Coolant;Eckert,1954

2. High temperature materials and hot structures;Frieß,2005

3. Effusion cooled CMC rocket combustion chamber;Hald,2005

4. Transpiration cooling at hypersonic flight - AKTiV on SHEFEX II;Böhrk,2014

5. Application of transpiration cooling for hot structures;Kuhn,2008

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2. Comparative analysis of compressible inviscid flow over symmetric and supercritical airfoil;Results in Physics;2024-07

3. Investigation on the effectiveness of transpiration cooling under the influence of shock wave;Applied Thermal Engineering;2024-01

4. Bayesian uncertainty quantification analysis of the SST model for transonic flow around airfoils simulation;Aerospace Science and Technology;2023-06

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