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Static-Thrust Tests of Six Rotor-Blade Designs on a Helicopter in the Langley Full-Scale TunnelNo abstract available
Document ID
19930093089
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Wartime Report
Authors
Dingeldein, Richard C. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Schaefer, Raymond F. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1945
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NACA-WR-L-101
NACA-ARR-L5F25b
Report Number: NACA-WR-L-101
Report Number: NACA-ARR-L5F25b
Accession Number
93R22379
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROTOR BLADES
PROPELLERS, HELICOPTER - THRUST, STATIC
HELICOPTERS - PERFORMANCE

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