Numerical Investigations of S-Shaped Air Inlet for Embedded Engines
Author:
Affiliation:
1. Federal University of Minas Gerais, 31270-901 Belo Horizonte, Brazil
2. Embraer S.A, 12246-160 Sao Jose dos Campos, Brazil
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B37256
Reference37 articles.
1. Wake ingestion propulsion benefit
2. Boundary Layer Ingestion Propulsion Benefit for Transport Aircraft
3. Computational Fluid Dynamics-Based Analysis of Boundary Layer Ingesting Propulsion
4. Flow control of a boundary layer ingesting serpentine diffuser via blowing and suction
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