Data for: "Engine-Airframe Integration - From Froude Theorem to Numerical Flow Simulation"
Abstract
This dataset contains the data of the intake maps for the underwing intake and the bli intake. The data corresponds to figure 9 of the manuscript. The intake maps are determined with the simulation software OpenFOAM. The results are given for the individual Mach numbers as the total pressure ratio over the non-dimensional mass flow parameter. The results are an addition to the result of the conference paper "Engine-Airframe Integration - From Froude Theorem to Numerical Flow Simulation" presented at EASN 2025. (2025-11-30)
Fields of Study & Subjects
Computational Fluid Dynamics and Aerodynamics
Fluid dynamics and aerodynamics studies
Turbomachinery Performance and Optimization
Publication details
- Journal / source
- Universitätsbibliothek Stuttgart
- Publication date
- 27 January 2026
- Language
- EN
- Document type
- Dataset