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Studies on wind tunnel straightenersTests using small-scale straighteners are reported. The studies allowed conclusions on the most favorable depth relationships, flow conditions behind the straightener and on the drag. The ways an obliquely hitting airflow is deflected by a straightener are examined. In addition the flow drag was measured and the manner in which the individual air columns emanating from the holes unite to form a homogeneous speed field was investigated.
Document ID
19820014410
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Schultz-Grunow, F.
(NASA Headquarters Washington, DC United States)
Wieghardt, K.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1982
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NAS 1.15:76689
NASA-TM-76689
Report Number: NAS 1.15:76689
Report Number: NASA-TM-76689
Accession Number
82N22284
Funding Number(s)
CONTRACT_GRANT: NASW-3541
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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