Adaptive Design Method for a Tilt-Rotor Engine Inlet Duct Optimization
Author:
Affiliation:
1. Koninklijk Nederlands Lucht- en Ruimtevaartcentrum
2. Leonardo SpA Divisione Elicotteri Cascina Costa
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-4019
Reference11 articles.
1. A high-order low-dispersion symmetry-preserving finite-volume method for compressible flow on curvilinear grids
2. Meheut, M., Sartor, F., Vergez, M., Laban, M., Schnell, R., Stuermer, A.W., and Lefevre, G. "Assessment of Fan/Airframe aerodynamic performance using 360° URANS computations: Code-to-Code comparison between ONERA, DLR, NLR and Airbus", AIAA 2019-0582.
3. Breakdown of aerodynamic interactions for the lateral rotors on a compound helicopter
4. SAE-ARP1420 C: Gas Turbine Engine Inlet Flow Distorsion Guidelines, Rev. C. April 2017.
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1. Investigation of the Internal Flow Characteristics of a Tiltrotor Aircraft Engine Inlet in a Gust Environment;Aerospace;2024-04-25
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