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The hemisphere-cylinder in dynamic pitch-up motionsLaser-Doppler velocimetry and seven-hole probes were employed to map out the velocity and vorticity field along a plane downstream of a hemisphere-cylinder. Steady flow data were obtained over a fixed model at a range of angles of attack, as well as over a model pitching through ramp motions to a final angle of attack. Attention was focused on the dynamic development of induced vortex asymmetry. It was found that the wake develops first in a symmetric fashion and asymmetry is generated with some time delay.
Document ID
19930064160
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Panzer, E. C.
(NASA Langley Research Center Hampton, VA, United States)
Rediniotis, O. K.
(NASA Langley Research Center Hampton, VA, United States)
Telionis, D. P.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, United States)
Date Acquired
August 16, 2013
Publication Date
July 1, 1993
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 93-2963
Report Number: AIAA PAPER 93-2963
Meeting Information
Meeting: AIAA, Fluid Dynamics Conference
Location: Orlando, FL
Country: United States
Start Date: July 6, 1993
End Date: July 9, 1993
Sponsors: AIAA
Accession Number
93A48157
Funding Number(s)
CONTRACT_GRANT: NAS1-18471
Distribution Limits
Public
Copyright
Other

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