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The effects of nose bluntness on the pressure fluctuations measured on 15 deg and 20 deg cone-cylinders at transonic speedsEffect of nose bluntness on pressure fluctuations measured on 15 deg and 20 deg cone cylinders at transonic speeds
Document ID
19650003491
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Coe, C. F. (NASA Ames Research Center Moffett Field, CA, United States)
Kaskey, A. J. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1963
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-779
Accession Number
65N13092
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CYLINDER
PRESSURE EFFECT
NOSE CONE
TRANSONIC SPEED

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