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Helicopter Design and Capability Trends as Seen from a Research Viewpoint Langley Research Center, NASA

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Gustafson, F. B., author.
Conference Name:
National Aerospace Engineering & Manufacturing Meeting
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1962
Summary:
Prospects for relief of the helicopter' s recognized problems by way of design changes as accompanied by, or resulting from, essential research-type information and understanding are examined. For example, the potential advantages of the nonarticulated rotor system are reviewed and the status of the required steps toward adequate knowledge of loads and dynamics is outlined. Other rotor configuration changes, as well as the basic topics of performance, dynamics, operating problems, and safety are similarly treated. It is concluded that many avenues are now available for basic improvements in helicopters via research and invention, while retaining the basic concept of low disc loadings
Notes:
Vendor supplied data
Publisher Number:
620297
Access Restriction:
Restricted for use by site license

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