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Dynamic Stability Investigation of Two Right Circular Cylinders in Axial Free Flight at Mach Numbers from 0.4 to 1.7 Fineness-ratio-2.56 Cylinder and Fineness-ratio-4.0 Cylinder with Flared AfterbodyDynamic longitudinal stability of right circular cylinders in axial free flight
Document ID
19660024023
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Mc Fall, J. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 28, 1957
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-L56L28
Accession Number
66N33313
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CIRCULAR CYLINDER
FREE FLIGHT
DYNAMIC STABILITY
LONGITUDINAL STABILITY

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