Optimization Study of the Dump Diffuser in Gas Turbine to Reduce Pressure Loss
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Analytics for US Patent No. 6807803, Gas turbine exhaust diffuser
As shown, air enters the diffuser of a jet engine at 18 kPa, 216 K with a velocity of 265 m/s, all data corresponding to high altitude flight. The air flows adiabatically
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Figure 3 from Diffuser Augmented Wind Turbine (DAWT) Technologies: A Review | Semantic Scholar
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Turbine Diffusers
A typical view of the gas turbine diffuser (1) and exhaust collector... | Download Scientific Diagram
Why does the diffuser section generate thrust in a jet engine? - Aviation Stack Exchange
Components of jet engines - Wikipedia
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Aircraft Gas Turbine Engine Diffuser
Computational study on multi-objective optimization of the diffuser augmented horizontal axis tidal turbine | SpringerLink
Energies | Free Full-Text | Upgrading a Shrouded Wind Turbine with a Self-Adaptive Flanged Diffuser
Energies | Free Full-Text | Power Output Enhancement of a Ducted Wind Turbine by Stabilizing Vortices around the Duct
Aircraft Turbine Engine Compressor Section and Compressor Types
IMPROVEMENT OF A TURBINE EXHAUST HOOD AND DIFFUSER PERFORMANCE WITHIN SPATIAL LIMITATIONS
Schematic view of a diffuser-shrouded wind turbine: (a) overview of... | Download Scientific Diagram
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Turbine Diffusers
Don't Let It Go To Waste - OPRA Gas Turbine
Characteristics of a highly efficient propeller type small wind turbine with a diffuser - ScienceDirect
Key Technologies for 1700℃ Class Ultra High Temperature Gas Turbine,Mitsubishi Heavy Industries Technical Review Vol.54 No.3(
Gas Turbine Tutorials: Gas Turbine Exhaust Frame and Diffuser