Numerical investigation of the effect of intake integration at transonic speeds on the DLR-F17E UCAV model for the TWG
Explore this paper's citation graph
- Type
- article
- Published
- 2010-02-01
- Cited by
- 1
- References
- 10
- OpenAlex
- https://openalex.org/W48678813
- Semantic Scholar
- https://api.semanticscholar.org/CorpusID:116828793
Keywords
Mach number, Transonic, Duct (anatomy), Mechanics, Pointwise
References
- Pre-Computations for the iGREEN Wing-Tailplane Interference Experiment in the TWG
- Efficiency Improvements of RANS-Based Analysis and Optimization using Implicit and Adjoint Methods on Unstructured Grids
- Development of the TAU-Code for aerospace applications
- Distinctive Features of the Turbulent Flow in a Trailing Vortex
- On the sensitization of turbulence models to rotation and curvature
- Calculation of Complex Three-Dimensional Configurations Employing the DLR-tau-Code
- Multigrid solution of the Navier-Stokes equations on triangular meshes
- Towards the Ultimate Conservative Difference Scheme
- Towards the ultimate conservative difference scheme V. A second-order sequel to Godunov's method
- A One-Equation Turbulence Model for Aerodynamic Flows
Cited by
Related papers
- Study of the influence of a highly integrated flow-through intake on compressible flows about the lambda wing configuration SACCON
- Generic Lambda Wing Configuration in Compressible Flow: Effect of Highly Integrated Intakes
- Effect of Angle of Attack on the Performance of Twin Intake Duct
- Aerodynamic Performance Comparison of High Power Turboprop S-Duct Intake on Channel Wing at Varying Azimuth
- Detailed Measurements on a Circular Cylinder in Cross Flow
- Numerical Investigation of Geometric Effects on Total Pressure Recovery of S-Ducts
- Mach number and freestream turbulence effects on turbine vane aerodynamic losses
- Experimental and computational analysis of a tangent ogive slender body at incompressible speeds
- RANS Simulations for Sensitivity Analysis of Compressor Transition Duct