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Accession Number ADA575657
Title Hover Testing of a Small-Scale Rotor with On-Blade Elevons.
Publication Date 1997
Media Count 12p
Personal Author M. V. Fulton R. A. Ormiston
Abstract A two-bladed, 7.5-ft diameter dynamic rotor model with 10% chord on- blade elevons driven by piezoceramic bimorph actuators was designed and tested in hover at tip speeds up to 298 ft/s. The elevon actuator succeeded in achieving deflections of plus or mi ...
Keywords Actuators
Aeroelasticity
Bending
Blades
Elevons
Excitation
Frequency
Frequency response
Hovering
Input
Loads(Forces)
Pitch(Motion)
Range(Extremes)
Rates
Response
Reynolds number
Rotors
Sweep frequency techniques
Test and evaluation
Torsion
Variations
Velocity
Vibration
Voltage
Wind tunnel tests

 
Source Agency Non Paid ADAS
NTIS Subject Category 51C - Aircraft
Corporate Author Army Aviation and Missile Command, Moffett Field, CA.
Document Type Technical report
Title Note N/A
NTIS Issue Number 1319
Contract Number N/A

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