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- W55165024 abstract "Abstract : A systematic research program to investigate the capability of the Lockheed-developed 'rigid' rotor system in the XH-51A helicopters is discussed. The primary objective of the research program was to attain level flight performance at a true airspeed of 200 knots; 210 knots true airspeed was actually attained with the Compound XH-51A. Analytical studies, design, fabrication and modification, laboratory tests, wind tunnel and ground tests, and research flight tests of two rotor configurations and a 'compound' version of the helicopter were performed." @default.
- W55165024 created "2016-06-24" @default.
- W55165024 creator A5007716641 @default.
- W55165024 date "1965-06-01" @default.
- W55165024 modified "2023-09-27" @default.
- W55165024 title "EXPLORATION OF HIGH-SPEED FLIGHT WITH THE XH-51A RIGID ROTOR HELICOPTER" @default.
- W55165024 doi "https://doi.org/10.21236/ad0617966" @default.
- W55165024 hasPublicationYear "1965" @default.
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