Characterization of Unsteadiness in an Overexpanded Planar Nozzle
Author:
Affiliation:
1. University of Campania Luigi Vanvitelli, 81031 Aversa, Italy
2. Sapienza University of Rome, 00184 Rome, Italy
Funder
Ministero dell’Istruzione, dell’Università e della Ricerca
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J057162
Reference41 articles.
1. Sea level side loads in high-area-ratio rocket engines
2. Nozzle flow separation
3. Side loads and thermal loads in rocket nozzles. Overview of the CNES-ONERA ATAC programme
4. Characteristic frequency and length scales in transonic diffuser flow oscillations
5. Experimental analysis of unsteady separated flows in a supersonic planar nozzle
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