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Application of transonic flow analysis to helicopter rotor problemsThe transonic aspect of helicopter flow analysis is addressed. The equations of motion and their implementations are examined, and the computation of real rotor flows is considered. Nonlifting rotor flows, high-speed hover, high advance ratio lifting rotor flows, and strong blade/vortex interaction computations are discussed.
Document ID
19900042832
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Caradonna, F. X. (NASA Ames Research Center; U.S. Army, Aeroflightdynamics Directorate, Moffett Field CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Aerodynamics
Accession Number
90A29887
Distribution Limits
Public
Copyright
Other

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