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The Wind-induced Loads on a Dynamically Scaled Model of a Large Missile in Launching PositionWind tunnel tests - effect of wind induced loads on dynamically scaled model of large missile in launching position
Document ID
19650018601
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Buell, D. A. (NASA Ames Research Center Moffett Field, CA, United States)
Kenyon, G. C. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1959
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-109
Report Number: NASA-TM-X-109
Accession Number
65N28202
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND EFFECT
SCALE MODEL
MISSILE
LAUNCHING PAD

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