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A wind-tunnel investigation at high subsonic speeds of the lateral control characteristics of various plain spoiler configurations on a 3-percent-thick 60 degree delta wingResults are presented of wind-tunnel investigations at Mach numbers of 0.60 to 0.94 and angles of attack of -2 degrees to about 24 degrees to determine the lateral control characteristics of spoilers with various wing chord-wise and spanwise locations and spoiler spans and deflections on thin 60 degree delta wing of NACA 65a003 airfoil section parallel to free stream.
Document ID
19930088380
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Wiley, Harleth G
Date Acquired
August 16, 2013
Publication Date
May 26, 1954
Report/Patent Number
NACA-RM-L54D01
Accession Number
93R17670
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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