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Inception length to a fully-developed fin-generated shock wave boundary-layer interactionAn experimental study of fin-generated shock wave turbulent boundary-layer interactions confirmed previous observations that, sufficiently far from the fin apex, such interactions become conical. The inception length to conical symmetry was found to increase weakly with Mach number for Mach numbers from 2.5 to 4 and fin angles from 4 to 22 deg. For the range of interactions examined, the inception length was found to depend primarily upon the inviscid shock angle, this angle ranging from 21 to 40 deg. The behavior of the inception length with shock angle can be broadly divided into two categories. For 'weak' interactions with shock angles less than about 35 deg, the inception length decreased as the shock angle increased. For 'strong' interactions with shock angles greater than about 35 deg, the inception region was small and was approximately constant at three boundary-layer thicknesses in length. In the latter, strong interaction case, the inception length was an order of magnitude smaller than that found in the weakest interactions examined, to the extent that strong interactions were practically fully-developed from the apex.
Document ID
19890054707
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lu, Frank K.
(Texas, University Arlington, United States)
Settles, Gary S.
(Pennsylvania State University University Park, United States)
Date Acquired
August 14, 2013
Publication Date
June 1, 1989
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 89-1850
Accession Number
89A42078
Funding Number(s)
CONTRACT_GRANT: AF-AFOSR-86-0082
CONTRACT_GRANT: NCA2-192
Distribution Limits
Public
Copyright
Other

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