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Evidence of surface waves and spreading of turbulence on ablating models.Surface modifications of recovered small-scale plastic models after high speed flight used to estimate extent of laminar and turbulent flow over surface related to ablation studies
Document ID
19660032270
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Wilkins, M. E.
Date Acquired
August 3, 2013
Publication Date
October 1, 1965
Publication Information
Publication: AIAA JOURNAL
Subject Category
Thermodynamics And Combustion
Accession Number
66A11560
Distribution Limits
Public
Copyright
Other
Keywords
ABLATING NOSE CONE
LAMINAR BOUNDARY LAYER
TURBULENT BOUNDARY LAYER
BOUNDARY LAYER TRANSITION

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