Hover Validation and Acoustic Baseline Blade Set
Hover Validation and Acoustic Baseline Blade Set
- New search for: Austin D Overmeyer
- New search for: Peter A Copp
- New search for: Norman W Schaeffler
- New search for: Austin D Overmeyer
- New search for: Peter A Copp
- New search for: Norman W Schaeffler
The Hover Validation and Acoustic Baseline (HVAB) blade set has been jointly developed by the U.S. Army Combat Capabilities Development Command Aviation & Missile Center (CCDC AvMC) and the NASA Revolutionary Vertical Lift Technology (RVLT) Project. This Mach-scale, 66.50 in radius, blade set will ultimately be tested in both hover and forward-flight to provide key data for analysis validation. This paper provides comprehensive detail of the blade geometry, instrumentation, and structure for use in future analyses.
Document information
Hover Validation and Acoustic Baseline Blade Set
2020-05-29
Report
No indication
English
Similar titles
The Prediction and Validation of Hover Performance and Detailed Blade Loads
| Online Contents | 2009
The Prediction and Validation of Hover Performance and Detailed Blade Loads
| British Library Conference Proceedings | 2008
The prediction and validation of hover performance and detailed blade loads
| Tema Archive | 2008
Optimization of S-76 rotor blade for hover performance
| AIAA | 2018
Velocity field of a lifting rotor blade in hover
| AIAA | 1988