NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

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

Back to Results
A forced-oscillation method for dynamic- stability testingSmall-amplitude forced oscillation technique for determining damping and oscillatory stability in roll, pitch, and yaw in free flight
Document ID
19640007102
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Averett, B. T. (NASA Langley Research Center Hampton, VA, United States)
Kilgore, R. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 2, 2013
Publication Date
March 10, 1964
Subject Category
Space Sciences
Accession Number
64N17016
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FREE FLIGHT
FORCED OSCILLATION
AERODYNAMIC STABILITY

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available