Our heavyweight helicopter equal in the world does not have
In Rostov started production of the most load-lifting rotary-wing car The Russian holding «Helicopt[...]
Special Recent Posts
In Italy broke experimental tiltrotor
The experimental military man конвертоплан, developed by "August Vestland's" company, brok[...]
The old plane — nonsense, pilots think - there was an attack
In spite of the fact that the main version of crash of the Russian plane of the Kogalymavia company [...]
The Israeli Apache will subject to peeling
The Israeli shock Boeing AH-64 Apache helicopters will undergo "peeling" procedure. As rep[...]
The aviation industry began to move
On Monday against Dubai Airshow air show - the 2015th Deputy Prime Minister Dmitry Rogozin blew up t[...]
Sitemap
Posts
- Category: Management and Minimisation of Uncertainties and Errors in Numerical Aerodynamics (continued)
- Coupling Methodology
- A Comparison of Fluid/Structure Coupling Methods for Reduced Structural Models
- Results of the FORM Analysis
- Sensitivity Analysis by a Global Variation in Structural Parameters
- Definition of the Limit State Function
- Combination of the FORM-Routine with Fluid-Structure Interaction Code Library
- First Order Reliability Method
- Part II: Stochastic Simulations
- Effect of Simplified Spar Cap and Rib Cap Modeling
- Idealization of Stiffened Structural Components
- General Simplifications Effect of the Element Offset
- Uncertainties due to Modeling Simplifications
- Design of the Wing Structure
- Part I: Model Uncertainties
- Quantification of Uncertainty
- Finite Element Models and Analysis Methods Used for Uncertainty Quantification
- Uncertainties of Numerical Structural Models in the Frame of Aeroelasticity
- Laminar Boundary Layer at High Reynolds Number
- Application Test Cases
- Numerical Results
- WENO Reconstruction on Unstructured Grids
- IDeC for Inhomogeneous Problems
- The Method of Iterated Defect Correction
- The Application of Iterated Defect Corrections Based on WENO Reconstruction
- DRA2303 Transonic Profile
- Oblique Shock on Flat Plate (SWBLI)
- Validation of STGM
- Sensor Validation
- Spille-Kaltenbach Control Planes
- Synthetic Turbulence Generation Methods (STGM)
- Sensor Development
- Numerical Methods
- Sensor Controlled Zonal RANS-LES Method
- Field of Application and Its Limits
- Industrial Application
- Applicability on Mixed Errors
- Boundary Layer
- Uncertainty Sensors
- Grid Expansion Ratio
- Grid Inclination
- Application of the Sensors
- Shocks
- Implementation of the Separation Sensor
- Separation
- Implementation of the Boundary Layer Sensor
- Boundary Layer
- Development ofthe Uncertainty Sensors
- Maximum Grid Expansion Ratio in the Boundary Layer Resolution
- Implementation of the y+ Sensor
- Wall Distance y+
- Implementation of the Inclinitation Sensor
- Orthogonality in the Boundary Layer
- Development of the Sensors
- Classification of Errors and Uncertainties
- Minimization and Quantification of Errors and Uncertainties in RANS Modeling
- Conclusion
- Mesh Modification with Anisotropic Quality Measures
- Mesh Manipulation
- TC 217
- DLR-F6
- Results
- Methods
- Application of Mesh Modifications and Adjoint Error Estimates
- Conclusions for the Application
- Error Indication Based on the Adjoint Solution
- Adjoint-Based Error Estimation and Functional Correction
- Results on Modified Grids
- Modification of Adapted Grids
- A Geometric Quality Measure for the Element Types of TAU
- Modification of Adapted Grids on the Base of a Geometrical Element Quality
- Improvements Using the Decomposability of Elements
- Quantification and Reduction of Numerical Uncertainties by Improvement of the TAU Grid Adaptation Tool and Adjoint Methods
- Application of Hexfine and Results
- Local Refinement of Hexahedra to Improve the Wake Discretisation
- Application and Results
- Grid Improvement Strategies and Techniques
- Application of the Error Indicator
- . Methods for the Detection of Improperly Discretised Grid Regions
- Effects of the Hybrid Border on the Flow Solution
- Uncertainties Induced by the Grid Topology
- Uncertainties Induced by Variation of the Trailing-Edge Geometry
- Numerical Method
- Identification of Sources of Error Induced by Geometry and Discretisation
- Methods and Strategies for the Detection and Management of Grid Induced Uncertainties in Numerical Aerodynamics
- Category: MECHANICS. OF FLIGHT
- Skin friction or Surface friction
- Numerical questions
- Scale effect and Reynolds Number
- Aerofoil data
- Sub-orbital flight - the aeroplane - missile - satellite
- Flights in space
- Re-entry into the atmosphere
- The return flight
- Orbiting the moon
- Launching a spacecraft
- Another way to the moon
- Going to the moon?
- Elliptical orbits
- Escape velocity and circular velocity
- The mechanics of circular orbits