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HUBSCHRAUBER
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3D Euler calculations of multibladed rotors in hover: investigation of the wake capturing properties
3D fatigue crack propagation analysis of a helicopter component
80 Vestas V80 in 6 Monaten. Offshore Projekt Horns Rev in Dänemark
3000-HP roller gear transmission development program, volume II. Design report
3000-HP Roller gear transmission development program. Volume III. Roller gear manufacture
3000-HP roller gear transmission development program. Volume (roem. 5) aircraft tiefdown testing
Ablösung der Blattaschenverklebungen an Rotorblättern
Abrasion-resistant canopy (ARC) materials evaluation project
Accurate estimation of object location in an image sequence using helicopter flight data
A centrifugal force actuated variable span morphing helicopter rotor
A characteristic time correlation for combustion inefficiency from alternative fuels
A comparison of coaxial and conventional rotor performance
A comparison of computational aeroacoustic prediction methods
A comparison of main rotor smoothing adjustments using linear and neural network algorithms
A comparison of measured and predicted XV-15 tiltrotor surface acoustic pressures
A comparison of nonlinear techniques for structural health monitoring
A comparison of stationary and non-stationary metrics for detecting faults in helicopter gearboxes
A comprehensive analytical model of rotorcraft aerodynamics and dynamics. Part 2: User's manual
A comprehensive analytical model of rotorcraft aerodynamics and dynamics. Part 3: Program manual
A comprehensive PIV measurement campaign on a fully equipped helicopter model
A comprehensive study of active microflaps for vibration reduction in rotorcraft
A computational analysis of parallel blade-vortex interactions using vorticity embedding
A computational study of BVI noise reduction using active twist control
A contribution to turbulence measurements with autonomous micro aerial vehicles
A contribution to vision-based autonomous helicopter flight in urban environments
A control system of the miniature helicopter with stereo-vision and time delay predictor
A correlation-based transition model using local variables for unstructured parallelized CFD codes
A coupled helicopter rotor/fuselage aeroelastic response model for ACSR
A coupled rotor/wing optimization procedure for high speed tilt-rotor aircraft
A coupled unstructured-adaptive cartesian CFD approach for hover prediction
Acoustical aspect of helicopter rotor blade flow instabilities
Acoustic cavity with active- passive segmented constrained layer damping treated panels
Acoustic characteristics of an isolated tiltrotor model in the DNW
Acoustic design of rotor blades using genetic algorithm
Acoustic locator system: Test results for the UH-1 and AH-1G(Technical memo. 1968-69)
Acoustic phasing, directionality and amplification effects of helicopter blade-vortex interactions