Constant altitude helicopter flight testing

dc.contributor.author	Layton, Donald M.
dc.contributor.author	Safe, Per
dc.date.accessioned	2021-04-28T23:39:05Z
dc.date.available	2021-04-28T23:39:05Z
dc.date.issued	1986
dc.description	AIAA/AHS/CASI/DGLR/IES/ISA/lTEA/SETP/SFTE 3rd Flight Testing Conference, April 2-4, 1986/Las Vegas, Nevada	en_US
dc.description.abstract	Normalized W/a performance data for a helicopter can be obtained during a constant altitude flight with the same accuracy as the ratio can be obtained during a variable density flight. The only bound on this method is that the data acquisition be as rapid as possible to minimize the weight change during the data acquisition phase.	en_US
dc.format.extent	6 p.
dc.identifier.citation	Layton, D. and Per Safe. "Constant altitude helicopter flight testing." 3rd Flight Testing Conference and Technical Display. 1986.	en_US
dc.identifier.uri	https://hdl.handle.net/10945/67007
dc.publisher	American Institute of Aeronautics and Astronautics (AIAA)
dc.rights	This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.	en_US
dc.title	Constant altitude helicopter flight testing	en_US
dc.type	Conference Paper	en_US
dspace.entity.type	Publication

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