Aeroacoustic Coupling Effect During the Ascent of Space Transportation Systems-Reference-Cited by-同舟云学术

Aeroacoustic Coupling Effect During the Ascent of Space Transportation Systems

Published:2021-07 Issue:7 Volume:59 Page:2346-2356
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Saile Dominik¹^ORCID,Gülhan Ali¹

Affiliation:

1. DLR, German Aerospace Center, 51147 Cologne, Germany

Funder

Deutsche Forschungsgemeinschaft

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J059747

Reference42 articles.

1. SaileD. “Experimental Analysis on Near-Wake Flows of Space Transportation Systems,” Ph.D. Thesis, Rheinisch-Westfälische Technische Hochschule Aachen, Aachen, Germany, 2019.

2. Effects of Exhaust Plume and Nozzle Length on Compressible Base Flows

3. Numerical Prediction and Experimental Validation of Unsteady Loads on ARIANE5 and VEGA

4. Reduced-order analysis of buffet flow of space launchers

5. Analysis of characteristic wake flow modes on a generic transonic backward-facing step configuration

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