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Flugmechanik
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Engine integration based on multi-disciplinary optimisation technique
Multidisciplinary conceptual design for aircraft with circulation control high-lift systems
The HART II international workshop: an assessment of the state of the art in CFD/CSD prediction
SFB 880: fundamentals of high lift for future commercial aircraft
Analysis of trimmable conditions for a civil aircraft with active high-lift system
Effect of an active high-lift system failure during landing approaches
Multidisciplinary analysis of CROR propulsion systems: DLR activities in the JTI SFWA project
Model order reduction for steady aerodynamics of high-lift configurations
Speeding-up the computation of high-lift aerodynamics using a residual-based reduced-order model
Numerical simulation of a regional train in cross-wind
Modification of Leishman-Beddoes model incorporating with a new trailing-edge vortex model
Conceptual Design and Experimental Demonstration of a Distributedly Actuated Morphing Wing
Underexpanded Jet Development from a Rectangular Nozzle with Aft-Deck
Metric-Based Mathematical Derivation of Efficient Airfoil Design Variables
Fundamental Solutions of the Potential Flow Equations for Rotorcraft with Applications
Supersonic Flow over a Shallow Open Rectangular Cavity
Unsteady Continuous Adjoint Approach for Aerodynamic Design on Dynamic Meshes
Multidimensional Flux Difference Splitting Schemes
Results from the Second AIAA CFD High-Lift Prediction Workshop Using Edge
Control of the Flexural Axis of a Wing with Piezoelectric Actuation
Lift Production by a Passively Flexible Rotating Wing
Development and Application of a New Unsteady Far-Field Drag Decomposition Method
Effect of Flutter on the Multidisciplinary Design Optimization of Truss-Braced-Wing Aircraft
Performance of Transition-Sensitive Models in Predicting Flow Structures over Delta Wings
Open/Closed-Loop Aeroservoelastic Predictions via Nonlinear, Reduced-Order Aerodynamic Models
Passive Attenuation of Modal Cavity Aeroacoustics Under Supersonic and Transonic Conditions
Overview and Summary of the Second AIAA High-Lift Prediction Workshop
Direct Evaluation of Acoustic-Intensity Vector Field Around an Impedance Scattering Body
A new method for design of fixed wing micro air vehicle
Analytical modeling of a cyclorotor in hovering state
NASA Trapezoidal Wing Computations Including Transition and Advanced Turbulence Modeling
Aerodynamic Measurements and Computational Analyses in Hypersonic Rarefied Flows
Effect of elastic deformation on the aerodynamic characteristics of a high-speed spinning projectile
Lagrangian Approach for Simulating Supercooled Large Droplets’ Impingement Effect
Flight Dynamics and Stability of Kites in Steady and Unsteady Wind Conditions
Time-Marching Considerations for Response Prediction of Structures in Hypersonic Flows
Nonlinear Aeroelastic Analysis with Inextensible Plate Theory Including Correlation with Experiment
Gust Load Alleviation for a Regional Aircraft Through a Static Output Feedback
Micro-vortex generators for shock wave/boundary layer interactions