Synonyme wurden verwendet für:
Prüfung
Suche ohne Synonyme:
keywords:("Prüfung")
Calculated performance, stability and maneuverability of high-speed tilting-prop-rotor aircraft
Correlation of SA349/2 helicopter flight-test data with a comprehensive rotorcraft model
Correlation of SA349/2 helicopter flight-test data with a comprehensive rotorcraft model
Calculated performance, stability, and maneuverability of high-speed tilting-prop-rotor aircraft
The effect of nonlinear elastomeric lag damper characteristics on helicopter rotor dynamics
Prediction of SA 349/2 GV blade loads in high speed flight using several rotor analyses
Hub and blade structural loads measurements of an SA349/2 helicopter
Correlation of SA349/2 Helicopter Flight Test Data with a Comprehensive Rotorcraft Model
Application of the joined wing to tiltrotor aircraft
Hub loads analysis of the SA349/2 helicopter
Full-scale investigation of aerodynamic interactions between a rotor and fuselage
Aeroelastic loads and stability investigation of a full-scale hingeless rotor
Overview of the Testing of a Small-Scale Proprotor
Overview of the Testing of a Small-Scale Proprotor
Analysis of Advanced Rotorcraft Configurations
Influence of Wake Models on Calculated Tiltrotor Aerodynamics
Vortex Wake Geometry of a Model Tilt Rotor in Forward Flight
Calculation of the Aerodynamic Behavior of the Tilt Rotor Aeroacoustic Model (TRAM) in the DNW
Application of a Slotted Airfoil for UH-60A Helicopter Performance
Airloads and Wake Geometry Calculations for an Isolated Tiltrotor Model in a Wind Tunnel
Measured Aerodynamic Interaction of Two Tiltrotors
Model for Vortex Ring State Influence on Rotorcraft Flight Dynamics
NASA Heavy Lift Rotorcraft Systems Investigation
Optimum Design of a Compound Helicopter
Designs and Technology Requirements for Civil Heavy Lift Rotorcraft
Aeromechanics Analysis of a Compound Helicopter
Performance and Design Investigation of Heavy Lift Tiltrotor with Aerodynamic Interference Effects
Performance of Advanced Heavy-Lift, High-Speed Rotorcraft Configurations
Influence of Lift Offset on Rotorcraft Performance
An Assessment of the State-of-the-art in Multidisciplinary Aeromechanical Analyses
Rotorcraft Conceptual Design Environment
Rotorcraft Conceptual Design Environment
NDARC - NASA Design and Analysis of Rotorcraft Validation and Demonstration
NDARC-NASA Design and Analysis of Rotorcraft Theoretical Basis and Architecture
Design of a Slowed-Rotor Compound Helicopter for Future Joint Service Missions
Design and Performance of Lift-Offset Rotorcraft for Short-Haul Missions
Conceptual Design and Performance Analysis for a Large Civil Compound Helicopter
Progress in Conceptual Design and Analysis of Advanced Rotorcraft
Application of Climate Impact Metrics to Rotorcraft Design
Application of Climate Impact Metrics to Civil Tiltrotor Design
Exploration of Configuration Options for a Large Civil Compound Helicopter
A History of Rotorcraft Comprehensive Analyses
Comparison of Computed and Measured Vortex Evolution for a UH-60A Rotor in Forward Flight
Conceptual Design of Vertical Lift Aircraft with Future Propulsion System Architectures
NDARC - NASA Design and Analysis of Rotorcraft
NDARC: NASA Design and Analysis of Rotorcraft
NDARC NASA Design and Analysis of Rotorcraft
NDARC NASA Design and Analysis of Rotorcraft
Coaxial Compound Helicopter for Confined Urban Operations
NDARC NASA Design and Analysis of Rotorcraft - Input, Appendix 4
Handling Qualities Optimization for Rotorcraft Conceptual Design
NDARC NASA Design and Analysis of Rotorcraft Theory Appendix 1
NDARC NASA Design and Analysis of Rotorcraft - Input, Appendix 2
Mars Helicopter Technology Demonstrator