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Newtonian aerodynamics for tangent ogive bodies of revolutionAerodynamic coefficients and static stability characteristics of tangent ogive bodies of revolution - lift-to-drag, and fineness ratios
Document ID
19650020584
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mayo, E. E. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-55235
X-671-65-244
Report Number: NASA-TM-X-55235
Report Number: X-671-65-244
Accession Number
65N30185
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC COEFFICIENT
ELLIPSOID
STATIC STABILITY
OGIVE

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