Rotating Detonation Wave Direction and the Influence of Nozzle Guide Vane Inclination
Author:
Affiliation:
1. Technische Universität Berlin, Germany
Funder
Bundesministerium für Wirtschaft und Energie
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060594
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1. Comprehensive Thermodynamic Analysis of the Humphrey Cycle for Gas Turbines with Pressure Gain Combustion
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