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Results of a study of Mach number and Reynolds number effects on the lee side vortex flow field characteristics of an ogive-cylinder-frustum-cylinder at angles of attack to 25 degrees, volume 1An experimental program was conducted to survey the lee side vortex flow field about an ogive-cylinder-frustum-cylinder at angles of attack to 25 degrees for two Reynolds numbers at Mach number 0.8, and one Reynolds number at Mach number 1.96. The data were obtained using miniature 5-port conical pressure probes calibrated for angle of attack and roll angle over a Mach number range of 0.6 to 3.0. The results are presented here as local flow field properties and circulation strengths for various body stations.
Document ID
19730006580
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Foley, J. E. (Chrysler Corp. New Orleans, LA, United States)
Date Acquired
September 2, 2013
Publication Date
October 31, 1972
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-123997-VOL-1
TN-AP-72-565-VOL-1
Report Number: NASA-CR-123997-VOL-1
Report Number: TN-AP-72-565-VOL-1
Accession Number
73N15307
Funding Number(s)
CONTRACT_GRANT: NAS8-24391
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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