Loading...
Please wait, while we are loading the content...
Similar Documents
Blade motion correlation for the full-scale uh-60a airloads rotor
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Barrows, Danny Romander, Ethan A. Meyn, Larry A. Burner Sr., Alpheus |
| Copyright Year | 2014 |
| Description | Testing was successfully completed in May 2010 on a full-scale UH-60A rotor system in the USAF's National Full-Scale Aerodynamics Complex (NFAC) 40- by 80-Foot Wind Tunnel.[1] The primary objective of this NASA Army sponsored test program was to acquire a comprehensive set of validation-quality measurements ona full-scale pressure-instrumented rotor system at conditions that challenge the most sophisticated modeling andsimulation tools. The test hardware included the same rotor blades used during the UH-60A Airloads flight test.[2] Key measurements included rotor performance, blade loads, blade pressures, blade displacements, and rotorwake measurements using large-field Particle Image Velocimetry (PIV) and Retro-reflective Background Oriented Schlieren (RBOS). |
| File Size | 403161 |
| Page Count | 4 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20140011305 |
| Archival Resource Key | ark:/13960/t7mq01r19 |
| Language | English |
| Publisher Date | 2014-01-22 |
| Access Restriction | Open |
| Subject Keyword | Airloads Rotor Full-scale Uh-60a Blade Motion Correlation Correlation Full Scale Tests Rotor Blades Turbomachinery Motion Simulation Uh-60a Helicopter Wind Tunnel Tests Bending Particle Image Velocimetry Torsion Displacement Aerodynamic Loads Loads Forces Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
