40 results on '"vortex lattice"'
Search Results
2. Nonlinear system identification of a UAV model with distributed aerodynamics and flexible structure
3. T-tail flutter simulations with regard to quadratic mode shape components
4. An improved high-lift aerodynamic prediction method for transport aircraft
5. Electrostatic charging of an aircraft due to airborne dust particles impacts
6. Dynamic maneuver loads calculations for a sailplane and comparison with flight test
7. A refined structural model for static aeroelastic response and divergence of metallic and composite wings
8. Extensions of prescribed wake modelling for helicopter rotor BVI noise investigations
9. Starting procedure of a flying wing for an airborne wind energy system: Starting procedure of a flying wing...
10. Acoustic and aerodynamic evaluation of DLR small-scale rotor configurations within GARTEUR AG26
11. Unsteady nonlinear lifting line model for active gust load alleviation of airplanes
12. A discussion on benchmarking unconventional configurations with conventional aircraft: the box-wing study case
13. A comparison of three conceptual design approaches applied to an electric distributed lift aircraft
14. Experimental investigation of UAV rotor aeroacoustics and aerodynamics with computational cross-validation
15. Aerodynamic modeling of a delta-wing UAV for model-based navigation
16. Trim Strategies and Dynamic Cross-Coupling During Aerial Refueling
17. Recent developments of common numerical methods and common experimental means within the framework of the large passenger aircraft program
18. Evaluation of the controllability of a remotely piloted high-altitude platform in atmospheric disturbances based on pilot-in-the-loop simulations
19. Flight mechanical analysis of a solar-powered high-altitude platform
20. Assessment of hydrogen transport aircraft: Effects of fuel tank integration
21. Aeroelastic method to investigate nonlinear elastic wing structures
22. Flight dynamics and control assessment for differential thrust aircraft in engine inoperative conditions including aero-propulsive effects
23. Comparison and evaluation of blade element methods against RANS simulations and test data
24. Design and development of a novel fixed-wing biplane micro air vehicle with enhanced static stability
25. Applying Eigenstructure Assignment to Inner-Loop Flight Control Laws for a Multibody Aircraft
26. Environmental life cycle assessment and operating cost analysis of a conceptual battery hybrid-electric transport aircraft
27. Development of a hardware-in-the-loop demonstrator for the validation of fault-tolerant control methods for a hybrid UAV
28. Structural design process and subsequent flight mechanical evaluation in preliminary aircraft design: demonstrated on passenger ride comfort assessment
29. Loads analysis and structural optimization of a high aspect ratio, composite wing aircraft
30. Load prediction of hingeless helicopter rotors including drivetrain dynamics
31. Co-design of aircraft vertical tail and control laws with distributed electric propulsion and flight envelop constraints
32. Advanced aeroelastic robust stability analysis with structural uncertainties
33. Design and sizing of an aeroelastic composite model for a flying wing configuration with maneuver, gust, and landing loads
34. Efficient and accurate technology for aircraft loads estimation
35. Verification of a low fidelity fast simulation framework through RANS simulations
36. Investigations of passive wing technologies for load reduction
37. The effects of a full-aircraft aerodynamic model on the design of a tailored composite wing
38. Wing aerostructural optimization with an analytical fuel consumption sensitivity model
39. Reduced-order models for aerodynamic applications, loads and MDO
40. An automated CFD analysis workflow in overall aircraft design applications
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