NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Experimental Investigation of the Damping in Roll of Cruciform Triangular Wing-body Combinations at Mach Numbers from 1.5 to 6.0
Document ID
19930088092
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Boissevain, Alfred G
Date Acquired
August 16, 2013
Publication Date
April 7, 1954
Report/Patent Number
NACA-RM-A54B15a
Report Number: NACA-RM-A54B15a
Accession Number
93R17382
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available