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Hover Validation and Acoustic Baseline Blade SetThe 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 ID
20205002153
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Austin D Overmeyer (United States Department of the Army Arlington, Virginia, United States)
Peter A Copp (United States Department of the Army Arlington, Virginia, United States)
Norman W Schaeffler (Langley Research Center Hampton, Virginia, United States)
Date Acquired
May 13, 2020
Publication Date
May 29, 2020
Publication Information
Subject Category
Aerodynamics
Funding Number(s)
CONTRACT_GRANT: ARMY / LaRC
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
Hover,Rotor,Helicopter,Aerodynamics,HVAB,PSP,AIAA Rotorcraft Simulation Working Group

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