Analysis of shock-wave unsteadiness in conical supersonic nozzles
Author:
Funder
Algerian Government
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference50 articles.
1. Numerical study of shock/boundary layer interaction in supersonic overexpanded nozzles;Hadjadj;Aerosp. Sci. Technol.,2002
2. Nozzle flow separation;Hadjadj;Shock Waves,2009
3. Assessment of transition regimes in a dual-bell nozzle and possibility of active fluidic control;Zmijanovic;Aerosp. Sci. Technol.,2018
4. Investigation of a transonic resonance with convergent–divergent nozzles;Zaman;J. Fluid Mech.,2002
5. Assessment of a hybrid RANS/LES simulation method and URANS method in depicting the unsteady motions of flow structures in a scramjet combustor;Han;Aerosp. Sci. Technol.,2018
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