Numerical Investigation of the Fluidic Adaptation of the Throat Cross-Section of Coanda Coflow Fluidic Thrust Vectoring Nozzles and on the Scalability Towards Mid-Sized Mixed Turbofan Engines
Veranstalter (Körperschaft):
American Institute of Aeronautics and Astronautics
Konferenztitel:
AIAA Aviation and Aeronautics Forum and Exposition (2025, Las Vegas, Nev.)