NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Low-Speed Investigation of the Effects of Frequency and Amplitude of Oscillation in Sideslip on the Lateral Stability Derivatives of a 60 D Delta Wing, a 45 D Sweptback Wing, and an Unswept Wing
Document ID
19930090030
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Lichtenstein, Jacob H
Williams, James L
Date Acquired
August 29, 2013
Publication Date
June 5, 1958
Report/Patent Number
NACA-RM-L58B26
Accession Number
93R19320
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available