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Introductory remarksSuggested fluid mechanics research to be conducted in the National Transonic Facility include: wind tunnel calibration; flat plate skin friction, flow visualization and measurement techniques; leading edge separation; high angle of attack separation; shock-boundary layer interaction; submarine shapes; low speed studies of cylinder normal to flow; and wall interference effects. These theoretical aerodynamic investigations will provide empirical inputs or validation data for computational aerodynamics, and increase the usefulness of existing wind tunnels.
Document ID
19770020202
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gessow, A.
(NASA Headquarters Washington, DC United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1977
Publication Information
Publication: NASA Langley Res. Center High Reynolds Number Res.
Subject Category
Research And Support Facilities (Air)
Accession Number
77N27146
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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